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reorganize file structure

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This commit is contained in:
Anthony Correa
2010-04-17 12:00:00 -05:00
parent 0da2092d89
commit 5bacd30bad
515 changed files with 2257 additions and 37 deletions
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xflr/outputs/.DS_Store vendored Executable file
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53
xflr/outputs/FDR001 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR001
Wing polar name : kickin' ass
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.006842 0.000251 0.000000 0.000251 0.000000 -0.026050 0.000000 -0.000000 -0.000000 9.7536 0.4046
-0.900 0.011881 0.000243 0.000000 0.000243 -0.000000 -0.032028 0.000000 0.000000 0.000000 9.7536 0.2865
-0.800 0.017486 0.000242 0.000000 0.000242 0.000000 -0.038399 -0.000000 -0.000000 -0.000000 9.7536 0.2333
-0.700 0.023090 0.000245 0.000000 0.000245 0.000000 -0.044770 0.000000 -0.000000 -0.000000 9.7536 0.2060
-0.600 0.028695 0.000252 0.000000 0.000252 0.000000 -0.051140 0.000000 -0.000000 -0.000000 9.7536 0.1894
-0.500 0.034863 0.000267 0.000000 0.000267 -0.000000 -0.057902 0.000000 0.000000 0.000000 9.7536 0.1765
-0.400 0.039903 0.000279 0.000000 0.000279 0.000000 -0.063881 0.000000 -0.000000 -0.000000 9.7536 0.1701
-0.300 0.045507 0.000300 0.000000 0.000300 -0.000000 -0.070251 -0.000000 0.000000 0.000000 9.7536 0.1640
-0.200 0.051111 0.000325 0.000000 0.000325 0.000000 -0.076621 0.000000 0.000000 0.000000 9.7536 0.1593
-0.100 0.056714 0.000354 0.000000 0.000354 -0.000000 -0.082991 0.000000 -0.000000 -0.000000 9.7536 0.1555
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0.200 0.073522 0.000467 0.000000 0.000467 -0.000000 -0.102097 -0.000000 -0.000000 -0.000000 9.7536 0.1475
0.300 0.079124 0.000514 0.000000 0.000514 0.000000 -0.108464 0.000000 -0.000000 -0.000000 9.7536 0.1456
0.400 0.084725 0.000565 0.000000 0.000565 -0.000000 -0.114831 -0.000000 -0.000000 -0.000000 9.7536 0.1440
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0.700 0.101523 0.000744 0.000000 0.000744 -0.000000 -0.133926 -0.000000 -0.000000 -0.000000 9.7536 0.1402
0.710 0.102066 0.000751 0.000000 0.000751 0.000000 -0.134543 0.000000 -0.000000 -0.000000 9.7536 0.1401
0.800 0.107121 0.000813 0.000000 0.000813 0.000000 -0.140289 -0.000000 -0.000000 -0.000000 9.7536 0.1391
0.900 0.112718 0.000886 0.000000 0.000886 0.000000 -0.146650 0.000000 -0.000000 -0.000000 9.7536 0.1382
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1.100 0.123909 0.001045 0.000000 0.001045 -0.000000 -0.159370 0.000000 -0.000000 -0.000000 9.7536 0.1367
1.200 0.129502 0.001131 0.000000 0.001131 0.000000 -0.165728 0.000000 -0.000000 -0.000000 9.7536 0.1360
1.300 0.135095 0.001221 0.000000 0.001221 0.000000 -0.172084 0.000000 -0.000000 -0.000000 9.7536 0.1354
1.400 0.140686 0.001316 0.000000 0.001316 0.000000 -0.178439 0.000000 -0.000000 -0.000000 9.7536 0.1348
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1.800 0.163037 0.001738 0.000000 0.001738 -0.000000 -0.203842 -0.000000 -0.000000 -0.000000 9.7536 0.1329
1.900 0.168621 0.001854 0.000000 0.001854 0.000000 -0.210188 0.000000 0.000000 0.000000 9.7536 0.1325
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2.300 0.190940 0.002364 0.000000 0.002364 -0.000000 -0.235552 -0.000000 0.000000 0.000000 9.7536 0.1312
2.400 0.196515 0.002502 0.000000 0.002502 0.000000 -0.241888 -0.000000 -0.000000 -0.000000 9.7536 0.1309
2.500 0.202648 0.002657 0.000000 0.002657 0.000000 -0.248606 -0.000000 -0.000000 -0.000000 9.7536 0.1305
2.600 0.207659 0.002791 0.000000 0.002791 -0.000000 -0.254551 -0.000000 -0.000000 -0.000000 9.7536 0.1304
2.700 0.213229 0.002942 0.000000 0.002942 0.000000 -0.260879 0.000000 -0.000000 -0.000000 9.7536 0.1301
2.800 0.218796 0.003097 0.000000 0.003097 -0.000000 -0.267205 0.000000 -0.000000 -0.000000 9.7536 0.1299
2.900 0.224360 0.003257 0.000000 0.003257 -0.000000 -0.273528 -0.000000 -0.000000 -0.000000 9.7536 0.1297
3.000 0.230482 0.003436 0.000000 0.003436 0.000000 -0.280232 0.000000 -0.000000 -0.000000 9.7536 0.1293

53
xflr/outputs/FDR001.out Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR001
Wing polar name : kickin' ass
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.006842 0.000251 0.000000 0.000251 0.000000 -0.026050 0.000000 -0.000000 -0.000000 9.7536 0.4046
-0.900 0.011881 0.000243 0.000000 0.000243 -0.000000 -0.032028 0.000000 0.000000 0.000000 9.7536 0.2865
-0.800 0.017486 0.000242 0.000000 0.000242 0.000000 -0.038399 -0.000000 -0.000000 -0.000000 9.7536 0.2333
-0.700 0.023090 0.000245 0.000000 0.000245 0.000000 -0.044770 0.000000 -0.000000 -0.000000 9.7536 0.2060
-0.600 0.028695 0.000252 0.000000 0.000252 0.000000 -0.051140 0.000000 -0.000000 -0.000000 9.7536 0.1894
-0.500 0.034863 0.000267 0.000000 0.000267 -0.000000 -0.057902 0.000000 0.000000 0.000000 9.7536 0.1765
-0.400 0.039903 0.000279 0.000000 0.000279 0.000000 -0.063881 0.000000 -0.000000 -0.000000 9.7536 0.1701
-0.300 0.045507 0.000300 0.000000 0.000300 -0.000000 -0.070251 -0.000000 0.000000 0.000000 9.7536 0.1640
-0.200 0.051111 0.000325 0.000000 0.000325 0.000000 -0.076621 0.000000 0.000000 0.000000 9.7536 0.1593
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0.100 0.067920 0.000425 0.000000 0.000425 0.000000 -0.095729 0.000000 0.000000 0.000000 9.7536 0.1497
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0.300 0.079124 0.000514 0.000000 0.000514 0.000000 -0.108464 0.000000 -0.000000 -0.000000 9.7536 0.1456
0.400 0.084725 0.000565 0.000000 0.000565 -0.000000 -0.114831 -0.000000 -0.000000 -0.000000 9.7536 0.1440
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0.700 0.101523 0.000744 0.000000 0.000744 -0.000000 -0.133926 -0.000000 -0.000000 -0.000000 9.7536 0.1402
0.710 0.102066 0.000751 0.000000 0.000751 0.000000 -0.134543 0.000000 -0.000000 -0.000000 9.7536 0.1401
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1.200 0.129502 0.001131 0.000000 0.001131 0.000000 -0.165728 0.000000 -0.000000 -0.000000 9.7536 0.1360
1.300 0.135095 0.001221 0.000000 0.001221 0.000000 -0.172084 0.000000 -0.000000 -0.000000 9.7536 0.1354
1.400 0.140686 0.001316 0.000000 0.001316 0.000000 -0.178439 0.000000 -0.000000 -0.000000 9.7536 0.1348
1.500 0.146838 0.001425 0.000000 0.001425 0.000000 -0.185180 0.000000 -0.000000 -0.000000 9.7536 0.1340
1.600 0.151864 0.001518 0.000000 0.001518 -0.000000 -0.191144 0.000000 -0.000000 -0.000000 9.7536 0.1338
1.700 0.157451 0.001626 0.000000 0.001626 0.000000 -0.197494 0.000000 -0.000000 -0.000000 9.7536 0.1333
1.800 0.163037 0.001738 0.000000 0.001738 -0.000000 -0.203842 -0.000000 -0.000000 -0.000000 9.7536 0.1329
1.900 0.168621 0.001854 0.000000 0.001854 0.000000 -0.210188 0.000000 0.000000 0.000000 9.7536 0.1325
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2.200 0.185363 0.002230 0.000000 0.002230 0.000000 -0.229214 -0.000000 -0.000000 -0.000000 9.7536 0.1315
2.300 0.190940 0.002364 0.000000 0.002364 -0.000000 -0.235552 -0.000000 0.000000 0.000000 9.7536 0.1312
2.400 0.196515 0.002502 0.000000 0.002502 0.000000 -0.241888 -0.000000 -0.000000 -0.000000 9.7536 0.1309
2.500 0.202648 0.002657 0.000000 0.002657 0.000000 -0.248606 -0.000000 -0.000000 -0.000000 9.7536 0.1305
2.600 0.207659 0.002791 0.000000 0.002791 -0.000000 -0.254551 -0.000000 -0.000000 -0.000000 9.7536 0.1304
2.700 0.213229 0.002942 0.000000 0.002942 0.000000 -0.260879 0.000000 -0.000000 -0.000000 9.7536 0.1301
2.800 0.218796 0.003097 0.000000 0.003097 -0.000000 -0.267205 0.000000 -0.000000 -0.000000 9.7536 0.1299
2.900 0.224360 0.003257 0.000000 0.003257 -0.000000 -0.273528 -0.000000 -0.000000 -0.000000 9.7536 0.1297
3.000 0.230482 0.003436 0.000000 0.003436 0.000000 -0.280232 0.000000 -0.000000 -0.000000 9.7536 0.1293

53
xflr/outputs/FDR001.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR001
Wing polar name : kickin' ass
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.006842 0.000251 0.000000 0.000251 0.000000 -0.026050 0.000000 -0.000000 -0.000000 9.7536 0.4046
-0.900 0.011881 0.000243 0.000000 0.000243 -0.000000 -0.032028 0.000000 0.000000 0.000000 9.7536 0.2865
-0.800 0.017486 0.000242 0.000000 0.000242 0.000000 -0.038399 -0.000000 -0.000000 -0.000000 9.7536 0.2333
-0.700 0.023090 0.000245 0.000000 0.000245 0.000000 -0.044770 0.000000 -0.000000 -0.000000 9.7536 0.2060
-0.600 0.028695 0.000252 0.000000 0.000252 0.000000 -0.051140 0.000000 -0.000000 -0.000000 9.7536 0.1894
-0.500 0.034863 0.000267 0.000000 0.000267 -0.000000 -0.057902 0.000000 0.000000 0.000000 9.7536 0.1765
-0.400 0.039903 0.000279 0.000000 0.000279 0.000000 -0.063881 0.000000 -0.000000 -0.000000 9.7536 0.1701
-0.300 0.045507 0.000300 0.000000 0.000300 -0.000000 -0.070251 -0.000000 0.000000 0.000000 9.7536 0.1640
-0.200 0.051111 0.000325 0.000000 0.000325 0.000000 -0.076621 0.000000 0.000000 0.000000 9.7536 0.1593
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0.000 0.062882 0.000392 0.000000 0.000392 0.000000 -0.089751 0.000000 -0.000000 -0.000000 9.7536 0.1516
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0.200 0.073522 0.000467 0.000000 0.000467 -0.000000 -0.102097 -0.000000 -0.000000 -0.000000 9.7536 0.1475
0.300 0.079124 0.000514 0.000000 0.000514 0.000000 -0.108464 0.000000 -0.000000 -0.000000 9.7536 0.1456
0.400 0.084725 0.000565 0.000000 0.000565 -0.000000 -0.114831 -0.000000 -0.000000 -0.000000 9.7536 0.1440
0.500 0.090889 0.000627 0.000000 0.000627 -0.000000 -0.121587 -0.000000 0.000000 0.000000 9.7536 0.1421
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0.700 0.101523 0.000744 0.000000 0.000744 -0.000000 -0.133926 -0.000000 -0.000000 -0.000000 9.7536 0.1402
0.710 0.102066 0.000751 0.000000 0.000751 0.000000 -0.134543 0.000000 -0.000000 -0.000000 9.7536 0.1401
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0.900 0.112718 0.000886 0.000000 0.000886 0.000000 -0.146650 0.000000 -0.000000 -0.000000 9.7536 0.1382
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1.100 0.123909 0.001045 0.000000 0.001045 -0.000000 -0.159370 0.000000 -0.000000 -0.000000 9.7536 0.1367
1.200 0.129502 0.001131 0.000000 0.001131 0.000000 -0.165728 0.000000 -0.000000 -0.000000 9.7536 0.1360
1.300 0.135095 0.001221 0.000000 0.001221 0.000000 -0.172084 0.000000 -0.000000 -0.000000 9.7536 0.1354
1.400 0.140686 0.001316 0.000000 0.001316 0.000000 -0.178439 0.000000 -0.000000 -0.000000 9.7536 0.1348
1.500 0.146838 0.001425 0.000000 0.001425 0.000000 -0.185180 0.000000 -0.000000 -0.000000 9.7536 0.1340
1.600 0.151864 0.001518 0.000000 0.001518 -0.000000 -0.191144 0.000000 -0.000000 -0.000000 9.7536 0.1338
1.700 0.157451 0.001626 0.000000 0.001626 0.000000 -0.197494 0.000000 -0.000000 -0.000000 9.7536 0.1333
1.800 0.163037 0.001738 0.000000 0.001738 -0.000000 -0.203842 -0.000000 -0.000000 -0.000000 9.7536 0.1329
1.900 0.168621 0.001854 0.000000 0.001854 0.000000 -0.210188 0.000000 0.000000 0.000000 9.7536 0.1325
2.000 0.174764 0.001987 0.000000 0.001987 0.000000 -0.216919 -0.000000 0.000000 0.000000 9.7536 0.1319
2.100 0.179784 0.002100 0.000000 0.002100 0.000000 -0.222875 0.000000 -0.000000 -0.000000 9.7536 0.1318
2.200 0.185363 0.002230 0.000000 0.002230 0.000000 -0.229214 -0.000000 -0.000000 -0.000000 9.7536 0.1315
2.300 0.190940 0.002364 0.000000 0.002364 -0.000000 -0.235552 -0.000000 0.000000 0.000000 9.7536 0.1312
2.400 0.196515 0.002502 0.000000 0.002502 0.000000 -0.241888 -0.000000 -0.000000 -0.000000 9.7536 0.1309
2.500 0.202648 0.002657 0.000000 0.002657 0.000000 -0.248606 -0.000000 -0.000000 -0.000000 9.7536 0.1305
2.600 0.207659 0.002791 0.000000 0.002791 -0.000000 -0.254551 -0.000000 -0.000000 -0.000000 9.7536 0.1304
2.700 0.213229 0.002942 0.000000 0.002942 0.000000 -0.260879 0.000000 -0.000000 -0.000000 9.7536 0.1301
2.800 0.218796 0.003097 0.000000 0.003097 -0.000000 -0.267205 0.000000 -0.000000 -0.000000 9.7536 0.1299
2.900 0.224360 0.003257 0.000000 0.003257 -0.000000 -0.273528 -0.000000 -0.000000 -0.000000 9.7536 0.1297
3.000 0.230482 0.003436 0.000000 0.003436 0.000000 -0.280232 0.000000 -0.000000 -0.000000 9.7536 0.1293

20
xflr/outputs/FDR004 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR004
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.085107 0.000981 0.000000 0.000981 0.000000 -0.142817 0.000000 -0.000000 -0.000000 9.7536 0.1523
-0.500 0.113515 0.001143 0.000000 0.001143 -0.000000 -0.175844 -0.000000 0.000000 0.000000 9.7536 0.1406
0.000 0.141908 0.001402 0.000000 0.001402 -0.000000 -0.208848 0.000000 0.000000 0.000000 9.7536 0.1336
0.500 0.170279 0.001759 0.000000 0.001759 -0.000000 -0.241821 0.000000 0.000000 0.000000 9.7536 0.1289
1.000 0.198620 0.002213 0.000000 0.002213 0.000000 -0.274753 0.000000 0.000000 0.000000 9.7536 0.1255
1.500 0.226925 0.002764 0.000000 0.002764 -0.000000 -0.307632 0.000000 -0.000000 -0.000000 9.7536 0.1231
2.000 0.255186 0.003411 0.000000 0.003411 0.000000 -0.340450 -0.000000 -0.000000 -0.000000 9.7536 0.1211
2.500 0.283396 0.004155 0.000000 0.004155 -0.000000 -0.373196 0.000000 -0.000000 -0.000000 9.7536 0.1196
3.000 0.311548 0.004994 0.000000 0.004994 -0.000000 -0.405860 0.000000 -0.000000 -0.000000 9.7536 0.1184

20
xflr/outputs/FDR004.out Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR004
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.085107 0.000981 0.000000 0.000981 0.000000 -0.142817 0.000000 -0.000000 -0.000000 9.7536 0.1523
-0.500 0.113515 0.001143 0.000000 0.001143 -0.000000 -0.175844 -0.000000 0.000000 0.000000 9.7536 0.1406
0.000 0.141908 0.001402 0.000000 0.001402 -0.000000 -0.208848 0.000000 0.000000 0.000000 9.7536 0.1336
0.500 0.170279 0.001759 0.000000 0.001759 -0.000000 -0.241821 0.000000 0.000000 0.000000 9.7536 0.1289
1.000 0.198620 0.002213 0.000000 0.002213 0.000000 -0.274753 0.000000 0.000000 0.000000 9.7536 0.1255
1.500 0.226925 0.002764 0.000000 0.002764 -0.000000 -0.307632 0.000000 -0.000000 -0.000000 9.7536 0.1231
2.000 0.255186 0.003411 0.000000 0.003411 0.000000 -0.340450 -0.000000 -0.000000 -0.000000 9.7536 0.1211
2.500 0.283396 0.004155 0.000000 0.004155 -0.000000 -0.373196 0.000000 -0.000000 -0.000000 9.7536 0.1196
3.000 0.311548 0.004994 0.000000 0.004994 -0.000000 -0.405860 0.000000 -0.000000 -0.000000 9.7536 0.1184

20
xflr/outputs/FDR004.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR004
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.085107 0.000981 0.000000 0.000981 0.000000 -0.142817 0.000000 -0.000000 -0.000000 9.7536 0.1523
-0.500 0.113515 0.001143 0.000000 0.001143 -0.000000 -0.175844 -0.000000 0.000000 0.000000 9.7536 0.1406
0.000 0.141908 0.001402 0.000000 0.001402 -0.000000 -0.208848 0.000000 0.000000 0.000000 9.7536 0.1336
0.500 0.170279 0.001759 0.000000 0.001759 -0.000000 -0.241821 0.000000 0.000000 0.000000 9.7536 0.1289
1.000 0.198620 0.002213 0.000000 0.002213 0.000000 -0.274753 0.000000 0.000000 0.000000 9.7536 0.1255
1.500 0.226925 0.002764 0.000000 0.002764 -0.000000 -0.307632 0.000000 -0.000000 -0.000000 9.7536 0.1231
2.000 0.255186 0.003411 0.000000 0.003411 0.000000 -0.340450 -0.000000 -0.000000 -0.000000 9.7536 0.1211
2.500 0.283396 0.004155 0.000000 0.004155 -0.000000 -0.373196 0.000000 -0.000000 -0.000000 9.7536 0.1196
3.000 0.311548 0.004994 0.000000 0.004994 -0.000000 -0.405860 0.000000 -0.000000 -0.000000 9.7536 0.1184

20
xflr/outputs/FDR005 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR005
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.085162 0.000927 0.000000 0.000927 -0.000000 -0.134114 0.000000 0.000000 0.000000 9.7536 0.1429
-0.500 0.113619 0.001087 0.000000 0.001087 0.000000 -0.165237 -0.000000 -0.000000 -0.000000 9.7536 0.1320
0.000 0.142061 0.001347 0.000000 0.001347 -0.000000 -0.196340 -0.000000 -0.000000 -0.000000 9.7536 0.1254
0.500 0.170480 0.001707 0.000000 0.001707 -0.000000 -0.227413 -0.000000 0.000000 0.000000 9.7536 0.1211
1.000 0.198870 0.002166 0.000000 0.002166 -0.000000 -0.258447 0.000000 0.000000 0.000000 9.7536 0.1179
1.500 0.227222 0.002724 0.000000 0.002724 -0.000000 -0.289432 0.000000 0.000000 0.000000 9.7536 0.1156
2.000 0.255529 0.003380 0.000000 0.003380 -0.000000 -0.320359 -0.000000 -0.000000 -0.000000 9.7536 0.1138
2.500 0.283785 0.004135 0.000000 0.004135 -0.000000 -0.351218 0.000000 -0.000000 -0.000000 9.7536 0.1124
3.000 0.311981 0.004988 0.000000 0.004988 -0.000000 -0.382000 0.000000 0.000000 0.000000 9.7536 0.1113

20
xflr/outputs/FDR005.out Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR005
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.085162 0.000927 0.000000 0.000927 -0.000000 -0.134114 0.000000 0.000000 0.000000 9.7536 0.1429
-0.500 0.113619 0.001087 0.000000 0.001087 0.000000 -0.165237 -0.000000 -0.000000 -0.000000 9.7536 0.1320
0.000 0.142061 0.001347 0.000000 0.001347 -0.000000 -0.196340 -0.000000 -0.000000 -0.000000 9.7536 0.1254
0.500 0.170480 0.001707 0.000000 0.001707 -0.000000 -0.227413 -0.000000 0.000000 0.000000 9.7536 0.1211
1.000 0.198870 0.002166 0.000000 0.002166 -0.000000 -0.258447 0.000000 0.000000 0.000000 9.7536 0.1179
1.500 0.227222 0.002724 0.000000 0.002724 -0.000000 -0.289432 0.000000 0.000000 0.000000 9.7536 0.1156
2.000 0.255529 0.003380 0.000000 0.003380 -0.000000 -0.320359 -0.000000 -0.000000 -0.000000 9.7536 0.1138
2.500 0.283785 0.004135 0.000000 0.004135 -0.000000 -0.351218 0.000000 -0.000000 -0.000000 9.7536 0.1124
3.000 0.311981 0.004988 0.000000 0.004988 -0.000000 -0.382000 0.000000 0.000000 0.000000 9.7536 0.1113

20
xflr/outputs/FDR005.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR005
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.085162 0.000927 0.000000 0.000927 -0.000000 -0.134114 0.000000 0.000000 0.000000 9.7536 0.1429
-0.500 0.113619 0.001087 0.000000 0.001087 0.000000 -0.165237 -0.000000 -0.000000 -0.000000 9.7536 0.1320
0.000 0.142061 0.001347 0.000000 0.001347 -0.000000 -0.196340 -0.000000 -0.000000 -0.000000 9.7536 0.1254
0.500 0.170480 0.001707 0.000000 0.001707 -0.000000 -0.227413 -0.000000 0.000000 0.000000 9.7536 0.1211
1.000 0.198870 0.002166 0.000000 0.002166 -0.000000 -0.258447 0.000000 0.000000 0.000000 9.7536 0.1179
1.500 0.227222 0.002724 0.000000 0.002724 -0.000000 -0.289432 0.000000 0.000000 0.000000 9.7536 0.1156
2.000 0.255529 0.003380 0.000000 0.003380 -0.000000 -0.320359 -0.000000 -0.000000 -0.000000 9.7536 0.1138
2.500 0.283785 0.004135 0.000000 0.004135 -0.000000 -0.351218 0.000000 -0.000000 -0.000000 9.7536 0.1124
3.000 0.311981 0.004988 0.000000 0.004988 -0.000000 -0.382000 0.000000 0.000000 0.000000 9.7536 0.1113

20
xflr/outputs/FDR006 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR006
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.091968 0.001738 0.000000 0.001738 0.000000 -0.160384 -0.000000 -0.000000 -0.000000 9.7536 0.1775
-0.500 0.120852 0.002090 0.000000 0.002090 -0.000000 -0.195204 -0.000000 0.000000 0.000000 9.7536 0.1643
0.000 0.149715 0.002561 0.000000 0.002561 0.000000 -0.230000 -0.000000 0.000000 0.000000 9.7536 0.1563
0.500 0.178548 0.003149 0.000000 0.003149 -0.000000 -0.264762 0.000000 0.000000 0.000000 9.7536 0.1509
1.000 0.207344 0.003856 0.000000 0.003856 -0.000000 -0.299477 -0.000000 0.000000 0.000000 9.7536 0.1470
1.500 0.236093 0.004680 0.000000 0.004680 -0.000000 -0.334137 -0.000000 0.000000 0.000000 9.7536 0.1440
2.000 0.264788 0.005620 0.000000 0.005620 -0.000000 -0.368730 -0.000000 0.000000 0.000000 9.7536 0.1418
2.500 0.293420 0.006677 0.000000 0.006677 -0.000000 -0.403246 -0.000000 0.000000 0.000000 9.7536 0.1399
3.000 0.321981 0.007850 0.000000 0.007850 -0.000000 -0.437675 0.000000 0.000000 0.000000 9.7536 0.1385

20
xflr/outputs/FDR006.out Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR006
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.091968 0.001738 0.000000 0.001738 0.000000 -0.160384 -0.000000 -0.000000 -0.000000 9.7536 0.1775
-0.500 0.120852 0.002090 0.000000 0.002090 -0.000000 -0.195204 -0.000000 0.000000 0.000000 9.7536 0.1643
0.000 0.149715 0.002561 0.000000 0.002561 0.000000 -0.230000 -0.000000 0.000000 0.000000 9.7536 0.1563
0.500 0.178548 0.003149 0.000000 0.003149 -0.000000 -0.264762 0.000000 0.000000 0.000000 9.7536 0.1509
1.000 0.207344 0.003856 0.000000 0.003856 -0.000000 -0.299477 -0.000000 0.000000 0.000000 9.7536 0.1470
1.500 0.236093 0.004680 0.000000 0.004680 -0.000000 -0.334137 -0.000000 0.000000 0.000000 9.7536 0.1440
2.000 0.264788 0.005620 0.000000 0.005620 -0.000000 -0.368730 -0.000000 0.000000 0.000000 9.7536 0.1418
2.500 0.293420 0.006677 0.000000 0.006677 -0.000000 -0.403246 -0.000000 0.000000 0.000000 9.7536 0.1399
3.000 0.321981 0.007850 0.000000 0.007850 -0.000000 -0.437675 0.000000 0.000000 0.000000 9.7536 0.1385

20
xflr/outputs/FDR006.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR006
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.091968 0.001738 0.000000 0.001738 0.000000 -0.160384 -0.000000 -0.000000 -0.000000 9.7536 0.1775
-0.500 0.120852 0.002090 0.000000 0.002090 -0.000000 -0.195204 -0.000000 0.000000 0.000000 9.7536 0.1643
0.000 0.149715 0.002561 0.000000 0.002561 0.000000 -0.230000 -0.000000 0.000000 0.000000 9.7536 0.1563
0.500 0.178548 0.003149 0.000000 0.003149 -0.000000 -0.264762 0.000000 0.000000 0.000000 9.7536 0.1509
1.000 0.207344 0.003856 0.000000 0.003856 -0.000000 -0.299477 -0.000000 0.000000 0.000000 9.7536 0.1470
1.500 0.236093 0.004680 0.000000 0.004680 -0.000000 -0.334137 -0.000000 0.000000 0.000000 9.7536 0.1440
2.000 0.264788 0.005620 0.000000 0.005620 -0.000000 -0.368730 -0.000000 0.000000 0.000000 9.7536 0.1418
2.500 0.293420 0.006677 0.000000 0.006677 -0.000000 -0.403246 -0.000000 0.000000 0.000000 9.7536 0.1399
3.000 0.321981 0.007850 0.000000 0.007850 -0.000000 -0.437675 0.000000 0.000000 0.000000 9.7536 0.1385

20
xflr/outputs/FDR007 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR007
Wing polar name : kickin' ass -inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.091190 0.001207 0.000000 0.001207 -0.000000 -0.163135 -0.000000 0.000000 0.000000 9.7536 0.1534
-0.500 0.120608 0.001405 0.000000 0.001405 0.000000 -0.199971 -0.000000 0.000000 0.000000 9.7536 0.1421
0.000 0.150010 0.001701 0.000000 0.001701 -0.000000 -0.236781 -0.000000 0.000000 0.000000 9.7536 0.1353
0.500 0.179388 0.002095 0.000000 0.002095 0.000000 -0.273556 0.000000 -0.000000 -0.000000 9.7536 0.1307
1.000 0.208736 0.002586 0.000000 0.002586 0.000000 -0.310284 -0.000000 -0.000000 -0.000000 9.7536 0.1274
1.500 0.238045 0.003175 0.000000 0.003175 0.000000 -0.346954 0.000000 0.000000 0.000000 9.7536 0.1250
2.000 0.267309 0.003860 0.000000 0.003860 -0.000000 -0.383554 -0.000000 -0.000000 -0.000000 9.7536 0.1230
2.500 0.296520 0.004642 0.000000 0.004642 0.000000 -0.420074 0.000000 0.000000 0.000000 9.7536 0.1215
3.000 0.325671 0.005520 0.000000 0.005520 0.000000 -0.456501 0.000000 0.000000 0.000000 9.7536 0.1203

20
xflr/outputs/FDR007.out Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR007
Wing polar name : kickin' ass -inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.091190 0.001207 0.000000 0.001207 -0.000000 -0.163135 -0.000000 0.000000 0.000000 9.7536 0.1534
-0.500 0.120608 0.001405 0.000000 0.001405 0.000000 -0.199971 -0.000000 0.000000 0.000000 9.7536 0.1421
0.000 0.150010 0.001701 0.000000 0.001701 -0.000000 -0.236781 -0.000000 0.000000 0.000000 9.7536 0.1353
0.500 0.179388 0.002095 0.000000 0.002095 0.000000 -0.273556 0.000000 -0.000000 -0.000000 9.7536 0.1307
1.000 0.208736 0.002586 0.000000 0.002586 0.000000 -0.310284 -0.000000 -0.000000 -0.000000 9.7536 0.1274
1.500 0.238045 0.003175 0.000000 0.003175 0.000000 -0.346954 0.000000 0.000000 0.000000 9.7536 0.1250
2.000 0.267309 0.003860 0.000000 0.003860 -0.000000 -0.383554 -0.000000 -0.000000 -0.000000 9.7536 0.1230
2.500 0.296520 0.004642 0.000000 0.004642 0.000000 -0.420074 0.000000 0.000000 0.000000 9.7536 0.1215
3.000 0.325671 0.005520 0.000000 0.005520 0.000000 -0.456501 0.000000 0.000000 0.000000 9.7536 0.1203

20
xflr/outputs/FDR007.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR007
Wing polar name : kickin' ass -inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.091190 0.001207 0.000000 0.001207 -0.000000 -0.163135 -0.000000 0.000000 0.000000 9.7536 0.1534
-0.500 0.120608 0.001405 0.000000 0.001405 0.000000 -0.199971 -0.000000 0.000000 0.000000 9.7536 0.1421
0.000 0.150010 0.001701 0.000000 0.001701 -0.000000 -0.236781 -0.000000 0.000000 0.000000 9.7536 0.1353
0.500 0.179388 0.002095 0.000000 0.002095 0.000000 -0.273556 0.000000 -0.000000 -0.000000 9.7536 0.1307
1.000 0.208736 0.002586 0.000000 0.002586 0.000000 -0.310284 -0.000000 -0.000000 -0.000000 9.7536 0.1274
1.500 0.238045 0.003175 0.000000 0.003175 0.000000 -0.346954 0.000000 0.000000 0.000000 9.7536 0.1250
2.000 0.267309 0.003860 0.000000 0.003860 -0.000000 -0.383554 -0.000000 -0.000000 -0.000000 9.7536 0.1230
2.500 0.296520 0.004642 0.000000 0.004642 0.000000 -0.420074 0.000000 0.000000 0.000000 9.7536 0.1215
3.000 0.325671 0.005520 0.000000 0.005520 0.000000 -0.456501 0.000000 0.000000 0.000000 9.7536 0.1203

20
xflr/outputs/FDR008 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR008
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.102761 0.001092 0.000000 0.001092 0.000000 -0.171934 -0.000000 -0.000000 -0.000000 9.7536 0.1434
-0.500 0.132184 0.001345 0.000000 0.001345 0.000000 -0.208771 -0.000000 -0.000000 -0.000000 9.7536 0.1354
0.000 0.161587 0.001696 0.000000 0.001696 0.000000 -0.245585 0.000000 -0.000000 -0.000000 9.7536 0.1303
0.500 0.190964 0.002145 0.000000 0.002145 0.000000 -0.282364 0.000000 -0.000000 -0.000000 9.7536 0.1267
1.000 0.220308 0.002692 0.000000 0.002692 -0.000000 -0.319097 0.000000 0.000000 0.000000 9.7536 0.1241
1.500 0.249610 0.003335 0.000000 0.003335 -0.000000 -0.355774 -0.000000 0.000000 0.000000 9.7536 0.1222
2.000 0.278864 0.004075 0.000000 0.004075 -0.000000 -0.392382 -0.000000 0.000000 0.000000 9.7536 0.1207
2.500 0.308063 0.004912 0.000000 0.004912 -0.000000 -0.428911 0.000000 0.000000 0.000000 9.7536 0.1194
3.000 0.337198 0.005845 0.000000 0.005845 0.000000 -0.465350 0.000000 -0.000000 -0.000000 9.7536 0.1184

20
xflr/outputs/FDR008.out Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR008
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.102761 0.001092 0.000000 0.001092 0.000000 -0.171934 -0.000000 -0.000000 -0.000000 9.7536 0.1434
-0.500 0.132184 0.001345 0.000000 0.001345 0.000000 -0.208771 -0.000000 -0.000000 -0.000000 9.7536 0.1354
0.000 0.161587 0.001696 0.000000 0.001696 0.000000 -0.245585 0.000000 -0.000000 -0.000000 9.7536 0.1303
0.500 0.190964 0.002145 0.000000 0.002145 0.000000 -0.282364 0.000000 -0.000000 -0.000000 9.7536 0.1267
1.000 0.220308 0.002692 0.000000 0.002692 -0.000000 -0.319097 0.000000 0.000000 0.000000 9.7536 0.1241
1.500 0.249610 0.003335 0.000000 0.003335 -0.000000 -0.355774 -0.000000 0.000000 0.000000 9.7536 0.1222
2.000 0.278864 0.004075 0.000000 0.004075 -0.000000 -0.392382 -0.000000 0.000000 0.000000 9.7536 0.1207
2.500 0.308063 0.004912 0.000000 0.004912 -0.000000 -0.428911 0.000000 0.000000 0.000000 9.7536 0.1194
3.000 0.337198 0.005845 0.000000 0.005845 0.000000 -0.465350 0.000000 -0.000000 -0.000000 9.7536 0.1184

20
xflr/outputs/FDR008.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR008
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.102761 0.001092 0.000000 0.001092 0.000000 -0.171934 -0.000000 -0.000000 -0.000000 9.7536 0.1434
-0.500 0.132184 0.001345 0.000000 0.001345 0.000000 -0.208771 -0.000000 -0.000000 -0.000000 9.7536 0.1354
0.000 0.161587 0.001696 0.000000 0.001696 0.000000 -0.245585 0.000000 -0.000000 -0.000000 9.7536 0.1303
0.500 0.190964 0.002145 0.000000 0.002145 0.000000 -0.282364 0.000000 -0.000000 -0.000000 9.7536 0.1267
1.000 0.220308 0.002692 0.000000 0.002692 -0.000000 -0.319097 0.000000 0.000000 0.000000 9.7536 0.1241
1.500 0.249610 0.003335 0.000000 0.003335 -0.000000 -0.355774 -0.000000 0.000000 0.000000 9.7536 0.1222
2.000 0.278864 0.004075 0.000000 0.004075 -0.000000 -0.392382 -0.000000 0.000000 0.000000 9.7536 0.1207
2.500 0.308063 0.004912 0.000000 0.004912 -0.000000 -0.428911 0.000000 0.000000 0.000000 9.7536 0.1194
3.000 0.337198 0.005845 0.000000 0.005845 0.000000 -0.465350 0.000000 -0.000000 -0.000000 9.7536 0.1184

21
xflr/outputs/FDR009 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sF DR009
Wing polar name : T1 -32.0 ft/s 0 0ft
Freestream speed : 3 2.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-2 0.028775 0.000902 0.039073 0.039975 0 -0.075392 0 0 0 9.7536 0.266
-1.5 0.055659 0.000888 0.039687 0.040574 0 -0.106895 0 0 0 9.7536 0.1949
-1 0.082543 0.00097 0.039993 0.040963 0 -0.138397 0 0 0 9.7536 0.1701
-0.5 0.109418 0.001148 0.045594 0.046742 0 -0.169891 0 0 0 9.7536 0.1575
0 0.136278 0.001422 0.049288 0.05071 0 -0.201364 0 0 0 9.7536 0.1499
0.5 0.163116 0.001792 0.051593 0.053384 0 -0.232805 0 0 0 9.7536 0.1448
1 0.189924 0.002257 0.054106 0.056363 0 -0.264205 0 0 0 9.7536 0.1412
1.5 0.216697 0.002817 0.057404 0.060221 0 -0.295557 0 0 0 9.7536 0.1384
2 0.243426 0.003472 0.05946 0.062932 0 -0.326849 0 0 0 9.7536 0.1363
2.5 0.270105 0.004222 0.062187 0.066409 0 -0.358073 0 0 0 9.7536 0.1346
3 0.296727 0.005065 0.064045 0.06911 0 -0.389217 0 0 0 9.7536 0.1333
3.5 0.323284 0.006002 0.066155 0.072157 0 -0.420274 0 0 0 9.7536 0.1321
4 0.34977 0.007031 0.070139 0.07717 0 -0.451235 0 0 0 9.7536 0.1312

1
xflr/outputs/FDR009.out Executable file
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QFLR5 v0.04 Beta

21
xflr/outputs/FDR009.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sF DR009
Wing polar name : T1 -32.0 ft/s 0 0ft
Freestream speed : 3 2.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-2 0.028775 0.000902 0.039073 0.039975 0 -0.075392 0 0 0 9.7536 0.266
-1.5 0.055659 0.000888 0.039687 0.040574 0 -0.106895 0 0 0 9.7536 0.1949
-1 0.082543 0.00097 0.039993 0.040963 0 -0.138397 0 0 0 9.7536 0.1701
-0.5 0.109418 0.001148 0.045594 0.046742 0 -0.169891 0 0 0 9.7536 0.1575
0 0.136278 0.001422 0.049288 0.05071 0 -0.201364 0 0 0 9.7536 0.1499
0.5 0.163116 0.001792 0.051593 0.053384 0 -0.232805 0 0 0 9.7536 0.1448
1 0.189924 0.002257 0.054106 0.056363 0 -0.264205 0 0 0 9.7536 0.1412
1.5 0.216697 0.002817 0.057404 0.060221 0 -0.295557 0 0 0 9.7536 0.1384
2 0.243426 0.003472 0.05946 0.062932 0 -0.326849 0 0 0 9.7536 0.1363
2.5 0.270105 0.004222 0.062187 0.066409 0 -0.358073 0 0 0 9.7536 0.1346
3 0.296727 0.005065 0.064045 0.06911 0 -0.389217 0 0 0 9.7536 0.1333
3.5 0.323284 0.006002 0.066155 0.072157 0 -0.420274 0 0 0 9.7536 0.1321
4 0.34977 0.007031 0.070139 0.07717 0 -0.451235 0 0 0 9.7536 0.1312

24
xflr/outputs/FDR010 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : FDR010s
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.116962 0.001621 0.051031 0.052652 -0.000000 -0.178726 -0.000000 0.000000 -0.000000 9.7536 0.1726
-0.500 0.143347 0.002042 0.056144 0.058186 0.000000 -0.207479 0.000000 0.000000 0.000000 9.7536 0.1635
0.000 0.169707 0.002565 0.058118 0.060682 -0.000000 -0.236203 -0.000000 0.000000 0.000000 9.7536 0.1572
0.500 0.196033 0.003189 0.059796 0.062985 -0.000000 -0.264890 0.000000 0.000000 0.000000 9.7536 0.1526
1.000 0.222318 0.003914 0.063433 0.067347 -0.000000 -0.293535 -0.000000 0.000000 0.000000 9.7536 0.1491
1.500 0.248556 0.004739 0.064884 0.069623 -0.000000 -0.322125 0.000000 0.000000 0.000000 9.7536 0.1464
2.000 0.274738 0.005665 0.066241 0.071906 0.000000 -0.350652 -0.000000 0.000000 -0.000000 9.7536 0.1442
2.500 0.300858 0.006689 0.067503 0.074192 0.000000 -0.379109 -0.000000 0.000000 0.000000 9.7536 0.1424
3.000 0.326908 0.007813 0.068834 0.076647 0.000000 -0.407487 -0.000000 0.000000 0.000000 9.7536 0.1410
3.500 0.352881 0.009034 0.070760 0.079794 0.000000 -0.435777 -0.000000 0.000000 -0.000000 9.7536 0.1397
4.000 0.378770 0.010353 0.075051 0.085405 0.000000 -0.463973 0.000000 0.000000 0.000000 9.7536 0.1387
4.500 0.404568 0.011768 0.082388 0.094156 -0.000000 -0.492068 -0.000000 0.000000 0.000000 9.7536 0.1378
5.000 0.430268 0.013279 0.082849 0.096128 0.000000 -0.520042 0.000000 0.000000 0.000000 9.7536 0.1370

24
xflr/outputs/FDR010.out Executable file
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QFLR5 v0.04 Beta
Wing name : FDR010s
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.116962 0.001621 0.051031 0.052652 -0.000000 -0.178726 -0.000000 0.000000 -0.000000 9.7536 0.1726
-0.500 0.143347 0.002042 0.056144 0.058186 0.000000 -0.207479 0.000000 0.000000 0.000000 9.7536 0.1635
0.000 0.169707 0.002565 0.058118 0.060682 -0.000000 -0.236203 -0.000000 0.000000 0.000000 9.7536 0.1572
0.500 0.196033 0.003189 0.059796 0.062985 -0.000000 -0.264890 0.000000 0.000000 0.000000 9.7536 0.1526
1.000 0.222318 0.003914 0.063433 0.067347 -0.000000 -0.293535 -0.000000 0.000000 0.000000 9.7536 0.1491
1.500 0.248556 0.004739 0.064884 0.069623 -0.000000 -0.322125 0.000000 0.000000 0.000000 9.7536 0.1464
2.000 0.274738 0.005665 0.066241 0.071906 0.000000 -0.350652 -0.000000 0.000000 -0.000000 9.7536 0.1442
2.500 0.300858 0.006689 0.067503 0.074192 0.000000 -0.379109 -0.000000 0.000000 0.000000 9.7536 0.1424
3.000 0.326908 0.007813 0.068834 0.076647 0.000000 -0.407487 -0.000000 0.000000 0.000000 9.7536 0.1410
3.500 0.352881 0.009034 0.070760 0.079794 0.000000 -0.435777 -0.000000 0.000000 -0.000000 9.7536 0.1397
4.000 0.378770 0.010353 0.075051 0.085405 0.000000 -0.463973 0.000000 0.000000 0.000000 9.7536 0.1387
4.500 0.404568 0.011768 0.082388 0.094156 -0.000000 -0.492068 -0.000000 0.000000 0.000000 9.7536 0.1378
5.000 0.430268 0.013279 0.082849 0.096128 0.000000 -0.520042 0.000000 0.000000 0.000000 9.7536 0.1370

24
xflr/outputs/FDR010.txt Executable file
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QFLR5 v0.04 Beta
Wing name : FDR010s
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.116962 0.001621 0.051031 0.052652 -0.000000 -0.178726 -0.000000 0.000000 -0.000000 9.7536 0.1726
-0.500 0.143347 0.002042 0.056144 0.058186 0.000000 -0.207479 0.000000 0.000000 0.000000 9.7536 0.1635
0.000 0.169707 0.002565 0.058118 0.060682 -0.000000 -0.236203 -0.000000 0.000000 0.000000 9.7536 0.1572
0.500 0.196033 0.003189 0.059796 0.062985 -0.000000 -0.264890 0.000000 0.000000 0.000000 9.7536 0.1526
1.000 0.222318 0.003914 0.063433 0.067347 -0.000000 -0.293535 -0.000000 0.000000 0.000000 9.7536 0.1491
1.500 0.248556 0.004739 0.064884 0.069623 -0.000000 -0.322125 0.000000 0.000000 0.000000 9.7536 0.1464
2.000 0.274738 0.005665 0.066241 0.071906 0.000000 -0.350652 -0.000000 0.000000 -0.000000 9.7536 0.1442
2.500 0.300858 0.006689 0.067503 0.074192 0.000000 -0.379109 -0.000000 0.000000 0.000000 9.7536 0.1424
3.000 0.326908 0.007813 0.068834 0.076647 0.000000 -0.407487 -0.000000 0.000000 0.000000 9.7536 0.1410
3.500 0.352881 0.009034 0.070760 0.079794 0.000000 -0.435777 -0.000000 0.000000 -0.000000 9.7536 0.1397
4.000 0.378770 0.010353 0.075051 0.085405 0.000000 -0.463973 0.000000 0.000000 0.000000 9.7536 0.1387
4.500 0.404568 0.011768 0.082388 0.094156 -0.000000 -0.492068 -0.000000 0.000000 0.000000 9.7536 0.1378
5.000 0.430268 0.013279 0.082849 0.096128 0.000000 -0.520042 0.000000 0.000000 0.000000 9.7536 0.1370

17
xflr/outputs/FDR012 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR012
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0.000 0.144128 0.001339 0.000000 0.001339 0.000000 -0.198932 -0.000000 -0.000000 -0.000000 9.7536 0.1202
1.000 0.202051 0.002148 0.000000 0.002148 0.000000 -0.262090 0.000000 0.000000 0.000000 9.7536 0.1130
2.000 0.259825 0.003355 0.000000 0.003355 0.000000 -0.325051 -0.000000 -0.000000 -0.000000 9.7536 0.1091
3.000 0.317389 0.004957 0.000000 0.004957 -0.000000 -0.387737 -0.000000 -0.000000 -0.000000 9.7536 0.1066
4.000 0.374686 0.006950 0.000000 0.006950 0.000000 -0.450073 0.000000 0.000000 0.000000 9.7536 0.1049
5.000 0.431657 0.009328 0.000000 0.009328 0.000000 -0.511982 -0.000000 -0.000000 -0.000000 9.7536 0.1037

17
xflr/outputs/FDR012.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR012
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0.000 0.144128 0.001339 0.000000 0.001339 0.000000 -0.198932 -0.000000 -0.000000 -0.000000 9.7536 0.1202
1.000 0.202051 0.002148 0.000000 0.002148 0.000000 -0.262090 0.000000 0.000000 0.000000 9.7536 0.1130
2.000 0.259825 0.003355 0.000000 0.003355 0.000000 -0.325051 -0.000000 -0.000000 -0.000000 9.7536 0.1091
3.000 0.317389 0.004957 0.000000 0.004957 -0.000000 -0.387737 -0.000000 -0.000000 -0.000000 9.7536 0.1066
4.000 0.374686 0.006950 0.000000 0.006950 0.000000 -0.450073 0.000000 0.000000 0.000000 9.7536 0.1049
5.000 0.431657 0.009328 0.000000 0.009328 0.000000 -0.511982 -0.000000 -0.000000 -0.000000 9.7536 0.1037

17
xflr/outputs/FDR013 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR013
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0.000 0.197841 0.002619 0.000000 0.002619 0.000000 -0.267136 -0.000000 -0.000000 -0.000000 9.7536 0.1217
1.000 0.254737 0.004020 0.000000 0.004020 -0.000000 -0.327464 -0.000000 -0.000000 -0.000000 9.7536 0.1159
2.000 0.311422 0.005817 0.000000 0.005817 0.000000 -0.387557 -0.000000 0.000000 0.000000 9.7536 0.1123
3.000 0.367837 0.008003 0.000000 0.008003 0.000000 -0.447341 0.000000 -0.000000 -0.000000 9.7536 0.1098
4.000 0.423924 0.010575 0.000000 0.010575 -0.000000 -0.506744 -0.000000 -0.000000 -0.000000 9.7536 0.1080
5.000 0.479626 0.013523 0.000000 0.013523 -0.000000 -0.565693 0.000000 -0.000000 -0.000000 9.7536 0.1067

14
xflr/outputs/FDR013.out Executable file
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QFLR5 v0.04 Beta
Wing name : sF DR013
Wing polar name : T1 -105.0 ft/ s-VLM2- 0. 00ft-Invisc id
Freestream speed : 10 4.990 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0 0.197841 0.002619 0 0.002619 0 -0.267136 0 0 0 32.001 0.1217
1 0.254737 0.00402 0 0.00402 0 -0.327464 0 0 0 32.001 0.1159
2 0.311422 0.005817 0 0.005817 0 -0.387557 0 0 0 32.001 0.1123
3 0.367837 0.008003 0 0.008003 0 -0.447341 0 0 0 32.001 0.1098
4 0.423924 0.010575 0 0.010575 0 -0.506744 0 0 0 32.001 0.108
5 0.479626 0.013523 0 0.013523 0 -0.565693 0 0 0 32.001 0.1067

17
xflr/outputs/FDR013.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR013
Wing polar name : T1-32.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0.000 0.197841 0.002619 0.000000 0.002619 0.000000 -0.267136 -0.000000 -0.000000 -0.000000 9.7536 0.1217
1.000 0.254737 0.004020 0.000000 0.004020 -0.000000 -0.327464 -0.000000 -0.000000 -0.000000 9.7536 0.1159
2.000 0.311422 0.005817 0.000000 0.005817 0.000000 -0.387557 -0.000000 0.000000 0.000000 9.7536 0.1123
3.000 0.367837 0.008003 0.000000 0.008003 0.000000 -0.447341 0.000000 -0.000000 -0.000000 9.7536 0.1098
4.000 0.423924 0.010575 0.000000 0.010575 -0.000000 -0.506744 -0.000000 -0.000000 -0.000000 9.7536 0.1080
5.000 0.479626 0.013523 0.000000 0.013523 -0.000000 -0.565693 0.000000 -0.000000 -0.000000 9.7536 0.1067

15
xflr/outputs/FDR020 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR020
Wing polar name : T1-32.0 ft/s-Panel- 0.31ft
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0.000 0.084447 0.000837 0.042292 0.043129 -0.000000 -0.036884 0.000000 -0.000000 -0.000000 9.7536 0.1450
1.000 0.121470 0.001267 0.048979 0.050246 0.000000 -0.036566 0.000000 -0.000000 -0.000000 9.7536 0.1286
2.000 0.158434 0.001864 0.053171 0.055035 -0.000000 -0.036226 0.000000 -0.000000 0.000000 9.7536 0.1198
3.000 0.195321 0.002624 0.058185 0.060809 -0.000000 -0.035866 0.000000 -0.000000 0.000000 9.7536 0.1144

15
xflr/outputs/FDR020.out Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR020
Wing polar name : T1-32.0 ft/s-Panel- 0.31ft
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0.000 0.084447 0.000837 0.042292 0.043129 -0.000000 -0.036884 0.000000 -0.000000 -0.000000 9.7536 0.1450
1.000 0.121470 0.001267 0.048979 0.050246 0.000000 -0.036566 0.000000 -0.000000 -0.000000 9.7536 0.1286
2.000 0.158434 0.001864 0.053171 0.055035 -0.000000 -0.036226 0.000000 -0.000000 0.000000 9.7536 0.1198
3.000 0.195321 0.002624 0.058185 0.060809 -0.000000 -0.035866 0.000000 -0.000000 0.000000 9.7536 0.1144

15
xflr/outputs/FDR020.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR020
Wing polar name : T1-32.0 ft/s-Panel- 0.31ft
Freestream speed : 32.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
0.000 0.084447 0.000837 0.042292 0.043129 -0.000000 -0.036884 0.000000 -0.000000 -0.000000 9.7536 0.1450
1.000 0.121470 0.001267 0.048979 0.050246 0.000000 -0.036566 0.000000 -0.000000 -0.000000 9.7536 0.1286
2.000 0.158434 0.001864 0.053171 0.055035 -0.000000 -0.036226 0.000000 -0.000000 0.000000 9.7536 0.1198
3.000 0.195321 0.002624 0.058185 0.060809 -0.000000 -0.035866 0.000000 -0.000000 0.000000 9.7536 0.1144

15
xflr/outputs/PDR001 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : whole damn thing scaled
Wing polar name : T1-16.0 ft/s-VLM2- 0.00ft
Freestream speed : 16.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-0.500 0.141086 0.003049 0.059669 0.062717 0.000000 -0.216817 -0.000000 -0.000000 0.000000 4.8768 0.1839
0.000 0.167846 0.003683 0.068042 0.071725 -0.000000 -0.245851 0.000000 -0.000000 -0.000000 4.8768 0.1752
0.500 0.194566 0.004440 0.071442 0.075882 -0.000000 -0.274840 0.000000 -0.000000 -0.000000 4.8768 0.1690
1.000 0.221238 0.005319 0.074465 0.079784 -0.000000 -0.303781 0.000000 -0.000000 -0.000000 4.8768 0.1643

15
xflr/outputs/PDR001.out Executable file
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QFLR5 v0.04 Beta
Wing name : whole damn thing scaled
Wing polar name : T1-16.0 ft/s-VLM2- 0.00ft
Freestream speed : 16.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-0.500 0.141086 0.003049 0.059669 0.062717 0.000000 -0.216817 -0.000000 -0.000000 0.000000 4.8768 0.1839
0.000 0.167846 0.003683 0.068042 0.071725 -0.000000 -0.245851 0.000000 -0.000000 -0.000000 4.8768 0.1752
0.500 0.194566 0.004440 0.071442 0.075882 -0.000000 -0.274840 0.000000 -0.000000 -0.000000 4.8768 0.1690
1.000 0.221238 0.005319 0.074465 0.079784 -0.000000 -0.303781 0.000000 -0.000000 -0.000000 4.8768 0.1643

15
xflr/outputs/PDR001.txt Executable file
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QFLR5 v0.04 Beta
Wing name : whole damn thing scaled
Wing polar name : T1-16.0 ft/s-VLM2- 0.00ft
Freestream speed : 16.000 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-0.500 0.141086 0.003049 0.059669 0.062717 0.000000 -0.216817 -0.000000 -0.000000 0.000000 4.8768 0.1839
0.000 0.167846 0.003683 0.068042 0.071725 -0.000000 -0.245851 0.000000 -0.000000 -0.000000 4.8768 0.1752
0.500 0.194566 0.004440 0.071442 0.075882 -0.000000 -0.274840 0.000000 -0.000000 -0.000000 4.8768 0.1690
1.000 0.221238 0.005319 0.074465 0.079784 -0.000000 -0.303781 0.000000 -0.000000 -0.000000 4.8768 0.1643

18
xflr/outputs/T1-105.0 ft s-VLM2- 0 2.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR012
Wing polar name : T1-105.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 104.990 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.086115 0.000931 0.000000 0.000931 0.000000 -0.135653 -0.000000 0.000000 0.000000 32.0010 0.1373
0.000 0.144128 0.001339 0.000000 0.001339 -0.000000 -0.198932 0.000000 0.000000 0.000000 32.0010 0.1202
1.000 0.202051 0.002148 0.000000 0.002148 -0.000000 -0.262090 -0.000000 -0.000000 -0.000000 32.0010 0.1130
2.000 0.259825 0.003355 0.000000 0.003355 -0.000000 -0.325051 0.000000 -0.000000 -0.000000 32.0010 0.1091
3.000 0.317390 0.004957 0.000000 0.004957 -0.000000 -0.387737 -0.000000 0.000000 0.000000 32.0010 0.1066
4.000 0.374686 0.006950 0.000000 0.006950 -0.000000 -0.450073 -0.000000 0.000000 0.000000 32.0010 0.1049
5.000 0.431657 0.009328 0.000000 0.009328 -0.000000 -0.511982 0.000000 -0.000000 -0.000000 32.0010 0.1037

18
xflr/outputs/T1-105.0 ft s-VLM2- 0.out Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR012
Wing polar name : T1-105.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 104.990 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.086115 0.000931 0.000000 0.000931 0.000000 -0.135653 -0.000000 0.000000 0.000000 32.0010 0.1373
0.000 0.144128 0.001339 0.000000 0.001339 -0.000000 -0.198932 0.000000 0.000000 0.000000 32.0010 0.1202
1.000 0.202051 0.002148 0.000000 0.002148 -0.000000 -0.262090 -0.000000 -0.000000 -0.000000 32.0010 0.1130
2.000 0.259825 0.003355 0.000000 0.003355 -0.000000 -0.325051 0.000000 -0.000000 -0.000000 32.0010 0.1091
3.000 0.317390 0.004957 0.000000 0.004957 -0.000000 -0.387737 -0.000000 0.000000 0.000000 32.0010 0.1066
4.000 0.374686 0.006950 0.000000 0.006950 -0.000000 -0.450073 -0.000000 0.000000 0.000000 32.0010 0.1049
5.000 0.431657 0.009328 0.000000 0.009328 -0.000000 -0.511982 0.000000 -0.000000 -0.000000 32.0010 0.1037

18
xflr/outputs/T1-105.0 ft s-VLM2- 0.txt Executable file
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QFLR5 v0.04 Beta
Wing name : sFDR012
Wing polar name : T1-105.0 ft/s-VLM2- 0.00ft-Inviscid
Freestream speed : 104.990 ft/s
alpha CL ICd PCd TCd CY Cm Rm Ym IYm QInf XCP
_________ ________ ________ _________ _________ _________ _________ _________ _________ _________ _________ _________
-1.000 0.086115 0.000931 0.000000 0.000931 0.000000 -0.135653 -0.000000 0.000000 0.000000 32.0010 0.1373
0.000 0.144128 0.001339 0.000000 0.001339 -0.000000 -0.198932 0.000000 0.000000 0.000000 32.0010 0.1202
1.000 0.202051 0.002148 0.000000 0.002148 -0.000000 -0.262090 -0.000000 -0.000000 -0.000000 32.0010 0.1130
2.000 0.259825 0.003355 0.000000 0.003355 -0.000000 -0.325051 0.000000 -0.000000 -0.000000 32.0010 0.1091
3.000 0.317390 0.004957 0.000000 0.004957 -0.000000 -0.387737 -0.000000 0.000000 0.000000 32.0010 0.1066
4.000 0.374686 0.006950 0.000000 0.006950 -0.000000 -0.450073 -0.000000 0.000000 0.000000 32.0010 0.1049
5.000 0.431657 0.009328 0.000000 0.009328 -0.000000 -0.511982 0.000000 -0.000000 -0.000000 32.0010 0.1037

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xflr/outputs/Trade Study planform/.DS_Store vendored Normal file
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xflr/outputs/Trade Study planform/FDR001.out Executable file
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xflr/outputs/Trade Study planform/FDR001.param Executable file
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xflr/outputs/Trade Study planform/FDR001.plan Executable file
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0 85 0 n00155sc.dat

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xflr/outputs/Trade Study planform/FDR001grimlite 2.tiff Executable file
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xflr/outputs/Trade Study planform/FDR001grimliteoutput 2.txt Executable file
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FDR001---------------------------------------------------
Wingspan: 140.000000, AR: 4.816577, Planform Area: 4069.280000, Wetted Area: 8408.002654
----------Takeoff--------------------------------
alfa: 9.392178, Cd0: 0.005688, CL: 0.662962, CD: 0.041996, CM: -0.788707, L/D: 15.786333
----------Cruise---------------------------------
alfa: 0.688827, Cd0: 0.004598, CL: 0.175574, CD: 0.007145, CM: -0.240396, L/D: 24.573681
----------Loiter---------------------------------
alfa: 3.765730, Cd0: 0.005328, CL: 0.347881, CD: 0.015325, CM: -0.434241, L/D: 22.699622
----------Landing--------------------------------
alfa: 7.172439, Cd0: 0.005688, CL: 0.538657, CD: 0.029657, CM: -0.648864, L/D: 18.162885

14
xflr/outputs/Trade Study planform/FDR001grimliteoutput.txt Executable file
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FDR001---------------------------------------------------
Wingspan: 140.000000, AR: 4.816577, Planform Area: 4069.280000, Wetted Area: 8408.002654
----------Takeoff--------------------------------
alfa: 9.392178, Cd0: 0.005688, CL: 0.662962, CD: 0.041996, CM: -0.788707, L/D: 15.786333
----------Cruise---------------------------------
alfa: 0.688827, Cd0: 0.004598, CL: 0.175574, CD: 0.007145, CM: -0.240396, L/D: 24.573681
----------Loiter---------------------------------
alfa: 3.765730, Cd0: 0.005328, CL: 0.347881, CD: 0.015325, CM: -0.434241, L/D: 22.699622
----------Landing--------------------------------
alfa: 7.172439, Cd0: 0.005688, CL: 0.538657, CD: 0.029657, CM: -0.648864, L/D: 18.162885

1
xflr/outputs/Trade Study planform/FDR002.out Executable file
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QFLR5 v0.04 Beta

1
xflr/outputs/Trade Study planform/FDR002.param Executable file
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1
xflr/outputs/Trade Study planform/FDR002.plan Executable file
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0 85 0 n00155sc.dat

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xflr/outputs/Trade Study planform/FDR002grimlite 2.tiff Executable file
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xflr/outputs/Trade Study planform/FDR002grimliteoutput 2.txt Executable file
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FDR002---------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 8.793252, Cd0: 0.005750, CL: 0.645215, CD: 0.032804, CM: -0.791355, L/D: 19.668736
----------Cruise---------------------------------
alfa: 0.471481, Cd0: 0.004640, CL: 0.170874, CD: 0.006538, CM: -0.242118, L/D: 26.135980
----------Loiter---------------------------------
alfa: 3.413484, Cd0: 0.005383, CL: 0.338569, CD: 0.012832, CM: -0.436290, L/D: 26.383862
----------Landing--------------------------------
alfa: 6.670833, Cd0: 0.005750, CL: 0.524237, CD: 0.023610, CM: -0.651275, L/D: 22.204057

14
xflr/outputs/Trade Study planform/FDR002grimliteoutput.txt Executable file
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FDR002---------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 8.793252, Cd0: 0.005750, CL: 0.645215, CD: 0.032804, CM: -0.791355, L/D: 19.668736
----------Cruise---------------------------------
alfa: 0.471481, Cd0: 0.004640, CL: 0.170874, CD: 0.006538, CM: -0.242118, L/D: 26.135980
----------Loiter---------------------------------
alfa: 3.413484, Cd0: 0.005383, CL: 0.338569, CD: 0.012832, CM: -0.436290, L/D: 26.383862
----------Landing--------------------------------
alfa: 6.670833, Cd0: 0.005750, CL: 0.524237, CD: 0.023610, CM: -0.651275, L/D: 22.204057

1
xflr/outputs/Trade Study planform/FDR003.out Executable file
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QFLR5 v0.04 Beta

1
xflr/outputs/Trade Study planform/FDR003.param Executable file
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laminarflow_to .40

1
xflr/outputs/Trade Study planform/FDR003.plan Executable file
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0 85 0 n00155sc.dat

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xflr/outputs/Trade Study planform/FDR003grimlite 2.tiff Executable file
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xflr/outputs/Trade Study planform/FDR003grimlite.tiff Executable file
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xflr/outputs/Trade Study planform/FDR003grimliteoutput 2.txt Executable file
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FDR003---------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 8.793252, Cd0: 0.005750, CL: 0.645215, CD: 0.032804, CM: -0.791355, L/D: 19.668736
----------Cruise---------------------------------
alfa: 0.471481, Cd0: 0.004640, CL: 0.170874, CD: 0.006538, CM: -0.242118, L/D: 26.135980
----------Loiter---------------------------------
alfa: 3.413484, Cd0: 0.005383, CL: 0.338569, CD: 0.012832, CM: -0.436290, L/D: 26.383862
----------Landing--------------------------------
alfa: 6.670833, Cd0: 0.005750, CL: 0.524237, CD: 0.023610, CM: -0.651275, L/D: 22.204057

14
xflr/outputs/Trade Study planform/FDR003grimliteoutput.txt Executable file
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FDR003---------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 8.793252, Cd0: 0.005750, CL: 0.645215, CD: 0.032804, CM: -0.791355, L/D: 19.668736
----------Cruise---------------------------------
alfa: 0.471481, Cd0: 0.004640, CL: 0.170874, CD: 0.006538, CM: -0.242118, L/D: 26.135980
----------Loiter---------------------------------
alfa: 3.413484, Cd0: 0.005383, CL: 0.338569, CD: 0.012832, CM: -0.436290, L/D: 26.383862
----------Landing--------------------------------
alfa: 6.670833, Cd0: 0.005750, CL: 0.524237, CD: 0.023610, CM: -0.651275, L/D: 22.204057

1
xflr/outputs/Trade Study planform/FDR004.out Executable file
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QFLR5 v0.04 Beta

1
xflr/outputs/Trade Study planform/FDR004.param Executable file
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7
xflr/outputs/Trade Study planform/FDR004.plan Executable file
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0 85 0 n00155sc.dat
2.32 82.73 2.36 n00155sc.dat
6.38 73.67 11.33 n00155sc.dat
14.2 52.13 30.6 n00155sc.dat
28.98 20 50 nasasc0714.dat
34.77 15 55 nasasc0714.dat
80 5 93 nasasc0714.dat

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xflr/outputs/Trade Study planform/FDR004grimlite 2.tiff Executable file
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xflr/outputs/Trade Study planform/FDR004grimlite.tiff Executable file
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xflr/outputs/Trade Study planform/FDR004grimliteoutput 2.txt Executable file
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FDR004---------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 8.985989, Cd0: 0.005750, CL: 0.645215, CD: 0.032804, CM: -0.793089, L/D: 19.668736
----------Cruise---------------------------------
alfa: 0.515615, Cd0: 0.004640, CL: 0.170874, CD: 0.006538, CM: -0.242515, L/D: 26.135980
----------Loiter---------------------------------
alfa: 3.510154, Cd0: 0.005383, CL: 0.338569, CD: 0.012832, CM: -0.437160, L/D: 26.383862
----------Landing--------------------------------
alfa: 6.825670, Cd0: 0.005750, CL: 0.524237, CD: 0.023610, CM: -0.652669, L/D: 22.204057

14
xflr/outputs/Trade Study planform/FDR004grimliteoutput.txt Executable file
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FDR004---------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 8.985989, Cd0: 0.005750, CL: 0.645215, CD: 0.032804, CM: -0.793089, L/D: 19.668736
----------Cruise---------------------------------
alfa: 0.515615, Cd0: 0.004640, CL: 0.170874, CD: 0.006538, CM: -0.242515, L/D: 26.135980
----------Loiter---------------------------------
alfa: 3.510154, Cd0: 0.005383, CL: 0.338569, CD: 0.012832, CM: -0.437160, L/D: 26.383862
----------Landing--------------------------------
alfa: 6.825670, Cd0: 0.005750, CL: 0.524237, CD: 0.023610, CM: -0.652669, L/D: 22.204057

1
xflr/outputs/Trade Study planform/FDR005.out Executable file
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QFLR5 v0.04 Beta

1
xflr/outputs/Trade Study planform/FDR005.param Executable file
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xflr/outputs/Trade Study planform/FDR005.plan Executable file
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0 85 0 n00155sc.dat
2.32 82.73 2.27 n00155sc.dat
6.38 73.67 11.33 n00155sc.dat
14.2 52.13 30.6 n00155sc.dat
28.98 20 45 nasasc0714.dat
34.77 15 50 nasasc0714.dat
80 5 89 nasasc0714.dat

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xflr/outputs/Trade Study planform/FDR005grimlite 2.tiff Executable file
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xflr/outputs/Trade Study planform/FDR005grimlite.tiff Executable file
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xflr/outputs/Trade Study planform/FDR005grimliteoutput 2.txt Executable file
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FDR005---------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 8.985989, Cd0: 0.005750, CL: 0.645215, CD: 0.032804, CM: -0.753131, L/D: 19.668736
----------Cruise---------------------------------
alfa: 0.515615, Cd0: 0.004640, CL: 0.170874, CD: 0.006538, CM: -0.227968, L/D: 26.135980
----------Loiter---------------------------------
alfa: 3.510154, Cd0: 0.005383, CL: 0.338569, CD: 0.012832, CM: -0.413630, L/D: 26.383862
----------Landing--------------------------------
alfa: 6.825670, Cd0: 0.005750, CL: 0.524237, CD: 0.023610, CM: -0.619192, L/D: 22.204057

14
xflr/outputs/Trade Study planform/FDR005grimliteoutput.txt Executable file
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FDR005---------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 8.985989, Cd0: 0.005750, CL: 0.645215, CD: 0.032804, CM: -0.753131, L/D: 19.668736
----------Cruise---------------------------------
alfa: 0.515615, Cd0: 0.004640, CL: 0.170874, CD: 0.006538, CM: -0.227968, L/D: 26.135980
----------Loiter---------------------------------
alfa: 3.510154, Cd0: 0.005383, CL: 0.338569, CD: 0.012832, CM: -0.413630, L/D: 26.383862
----------Landing--------------------------------
alfa: 6.825670, Cd0: 0.005750, CL: 0.524237, CD: 0.023610, CM: -0.619192, L/D: 22.204057

1
xflr/outputs/Trade Study planform/FDR006.out Executable file
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xflr/outputs/Trade Study planform/FDR006.param Executable file
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xflr/outputs/Trade Study planform/FDR006.plan Executable file
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0 85 0 n00155sc.dat
2.32 82.73 2.27 n00155sc.dat
6.38 73.67 11.33 n00155sc.dat
14.2 52.13 30.6 n00155sc.dat
28.98 25 55 nasasc0714.dat
34.77 20 60 nasasc0714.dat
80 10 82 nasasc0714.dat

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xflr/outputs/Trade Study planform/FDR006grimlite 2.tiff Executable file
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xflr/outputs/Trade Study planform/FDR006grimliteoutput 2.txt Executable file
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FDR006---------------------------------------------------
Wingspan: 160.000000, AR: 5.372164, Planform Area: 4765.305000, Wetted Area: 9841.204819
----------Takeoff--------------------------------
alfa: 7.300510, Cd0: 0.005716, CL: 0.566129, CD: 0.029454, CM: -0.726435, L/D: 19.220819
----------Cruise---------------------------------
alfa: -0.001232, Cd0: 0.004619, CL: 0.149930, CD: 0.006284, CM: -0.229916, L/D: 23.859484
----------Loiter---------------------------------
alfa: 2.580159, Cd0: 0.005354, CL: 0.297069, CD: 0.011890, CM: -0.405451, L/D: 24.985343
----------Landing--------------------------------
alfa: 5.438244, Cd0: 0.005716, CL: 0.459980, CD: 0.021387, CM: -0.599801, L/D: 21.507670

14
xflr/outputs/Trade Study planform/FDR006grimliteoutput.txt Executable file
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FDR006---------------------------------------------------
Wingspan: 160.000000, AR: 5.372164, Planform Area: 4765.305000, Wetted Area: 9841.204819
----------Takeoff--------------------------------
alfa: 7.300510, Cd0: 0.005716, CL: 0.566129, CD: 0.029454, CM: -0.726435, L/D: 19.220819
----------Cruise---------------------------------
alfa: -0.001232, Cd0: 0.004619, CL: 0.149930, CD: 0.006284, CM: -0.229916, L/D: 23.859484
----------Loiter---------------------------------
alfa: 2.580159, Cd0: 0.005354, CL: 0.297069, CD: 0.011890, CM: -0.405451, L/D: 24.985343
----------Landing--------------------------------
alfa: 5.438244, Cd0: 0.005716, CL: 0.459980, CD: 0.021387, CM: -0.599801, L/D: 21.507670

1
xflr/outputs/Trade Study planform/FDR007.out Executable file
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xflr/outputs/Trade Study planform/FDR007.param Executable file
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xflr/outputs/Trade Study planform/FDR007.plan Executable file
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0 85 0 n00155sc.dat
2.32 82.73 2.27 n00155sc.dat
6.38 73.67 11.33 n00155sc.dat
14.2 52.13 30.6 n00155sc.dat
28.98 20 55 nasasc0714.dat
34.77 15 60 nasasc0714.dat
80 7.5 92 nasasc0714.dat

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xflr/outputs/Trade Study planform/FDR007grimlite 2.tiff Executable file
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xflr/outputs/Trade Study planform/FDR007grimliteoutput 2.txt Executable file
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FDR007---------------------------------------------------
Wingspan: 160.000000, AR: 5.961418, Planform Area: 4294.280000, Wetted Area: 8871.044819
----------Takeoff--------------------------------
alfa: 8.245274, Cd0: 0.005754, CL: 0.628226, CD: 0.032095, CM: -0.830660, L/D: 19.573691
----------Cruise---------------------------------
alfa: 0.282329, Cd0: 0.004644, CL: 0.166375, CD: 0.006491, CM: -0.257328, L/D: 25.631038
----------Loiter---------------------------------
alfa: 3.097476, Cd0: 0.005387, CL: 0.329654, CD: 0.012640, CM: -0.460018, L/D: 26.080567
----------Landing--------------------------------
alfa: 6.214371, Cd0: 0.005754, CL: 0.510434, CD: 0.023143, CM: -0.684435, L/D: 22.055258

14
xflr/outputs/Trade Study planform/FDR007grimliteoutput.txt Executable file
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FDR007---------------------------------------------------
Wingspan: 160.000000, AR: 5.961418, Planform Area: 4294.280000, Wetted Area: 8871.044819
----------Takeoff--------------------------------
alfa: 8.245274, Cd0: 0.005754, CL: 0.628226, CD: 0.032095, CM: -0.830660, L/D: 19.573691
----------Cruise---------------------------------
alfa: 0.282329, Cd0: 0.004644, CL: 0.166375, CD: 0.006491, CM: -0.257328, L/D: 25.631038
----------Loiter---------------------------------
alfa: 3.097476, Cd0: 0.005387, CL: 0.329654, CD: 0.012640, CM: -0.460018, L/D: 26.080567
----------Landing--------------------------------
alfa: 6.214371, Cd0: 0.005754, CL: 0.510434, CD: 0.023143, CM: -0.684435, L/D: 22.055258

1
xflr/outputs/Trade Study planform/FDR008.out Executable file
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xflr/outputs/Trade Study planform/FDR008.param Executable file
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xflr/outputs/Trade Study planform/FDR008.plan Executable file
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0 85 0 n00155sc.dat

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xflr/outputs/Trade Study planform/FDR008grimlite 2.tiff Executable file
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xflr/outputs/Trade Study planform/FDR008grimliteoutput 2.txt Executable file
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FDR008---------------------------------------------------
Wingspan: 160.000000, AR: 5.961418, Planform Area: 4294.280000, Wetted Area: 8871.044819
----------Takeoff--------------------------------
alfa: 8.245274, Cd0: 0.005754, CL: 0.628226, CD: 0.032095, CM: -0.830660, L/D: 19.573691
----------Cruise---------------------------------
alfa: 0.282329, Cd0: 0.004644, CL: 0.166375, CD: 0.006491, CM: -0.257328, L/D: 25.631038
----------Loiter---------------------------------
alfa: 3.097476, Cd0: 0.005387, CL: 0.329654, CD: 0.012640, CM: -0.460018, L/D: 26.080567
----------Landing--------------------------------
alfa: 6.214371, Cd0: 0.005754, CL: 0.510434, CD: 0.023143, CM: -0.684435, L/D: 22.055258

14
xflr/outputs/Trade Study planform/FDR008grimliteoutput.txt Executable file
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FDR008---------------------------------------------------
Wingspan: 160.000000, AR: 5.961418, Planform Area: 4294.280000, Wetted Area: 8871.044819
----------Takeoff--------------------------------
alfa: 8.245274, Cd0: 0.005754, CL: 0.628226, CD: 0.032095, CM: -0.830660, L/D: 19.573691
----------Cruise---------------------------------
alfa: 0.282329, Cd0: 0.004644, CL: 0.166375, CD: 0.006491, CM: -0.257328, L/D: 25.631038
----------Loiter---------------------------------
alfa: 3.097476, Cd0: 0.005387, CL: 0.329654, CD: 0.012640, CM: -0.460018, L/D: 26.080567
----------Landing--------------------------------
alfa: 6.214371, Cd0: 0.005754, CL: 0.510434, CD: 0.023143, CM: -0.684435, L/D: 22.055258

1
xflr/outputs/Trade Study planform/FDR009.out Executable file
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xflr/outputs/Trade Study planform/FDR009.param Executable file
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xflr/outputs/Trade Study planform/FDR009.plan Executable file
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0 95 0 n00155sc.dat

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xflr/outputs/Trade Study planform/FDR009grimlite 2.tiff Executable file
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