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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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42
ronald-plus/Ronaldplus Outputs/FDR001.txt Executable file
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FDR001
Outputs--------------------------------------------------
Wingspan: 140.000000, AR: 4.816577, Planform Area: 4069.280000, Wetted Area: 8408.002654
----------Takeoff--------------------------------
alfa: 6.125000, Cd0: 0.009957, CL: 0.480000, CD: 0.028410, D: 10790.513767, CM: -0.582875, L/D: 15.932485
----------Cruise---------------------------------
alfa: 0.951405, Cd0: 0.005179, CL: 0.190279, CD: 0.007481, D: 6817.381579, CM: -0.256939, L/D: 25.434985
D_Wing:993.322998, D_fuselage:3770.664809
----------Loiter---------------------------------
alfa: 3.952095, Cd0: 0.005682, CL: 0.358317, CD: 0.013937, D: 5208.157173, CM: -0.445982, L/D: 25.709670
----------Landing--------------------------------
alfa: 4.714286, Cd0: 0.009735, CL: 0.401000, CD: 0.021135, D: 9997.294077, CM: -0.494000, L/D: 18.973583
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.056
cLalpha 0.056 cL0 0.137
cL0 0.137 cMalpha-0.063
cMalpha-0.063 cM0-0.197
cM0-0.197 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR002.txt Executable file
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FDR002
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 5.894737, Cd0: 0.009897, CL: 0.480000, CD: 0.024414, D: 9527.785965, CM: -0.600053, L/D: 18.540333
----------Cruise---------------------------------
alfa: 0.722547, Cd0: 0.005203, CL: 0.185185, CD: 0.006919, D: 6478.628035, CM: -0.258688, L/D: 26.764926
D_Wing:1155.571422, D_fuselage:3770.664809
----------Loiter---------------------------------
alfa: 3.591678, Cd0: 0.005699, CL: 0.348726, CD: 0.011851, D: 4550.243775, CM: -0.448051, L/D: 29.426995
----------Landing--------------------------------
alfa: 4.508772, Cd0: 0.009677, CL: 0.401000, CD: 0.018645, D: 9062.166794, CM: -0.508579, L/D: 21.507190
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.057
cLalpha 0.057 cL0 0.144
cL0 0.144 cMalpha-0.066
cMalpha-0.066 cM0-0.211
cM0-0.211 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR003.txt Executable file
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FDR003
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8646.272379
----------Takeoff--------------------------------
alfa: 5.894737, Cd0: 0.009903, CL: 0.480000, CD: 0.024420, D: 9530.278297, CM: -0.600053, L/D: 18.535485
----------Cruise---------------------------------
alfa: 0.722547, Cd0: 0.005208, CL: 0.185185, CD: 0.006924, D: 6483.328324, CM: -0.258688, L/D: 26.745522
D_Wing:1159.593905, D_fuselage:3771.626725
----------Loiter---------------------------------
alfa: 3.591678, Cd0: 0.005704, CL: 0.348726, CD: 0.011856, D: 4552.237898, CM: -0.448051, L/D: 29.414104
----------Landing--------------------------------
alfa: 4.508772, Cd0: 0.009684, CL: 0.401000, CD: 0.018651, D: 9065.211714, CM: -0.508579, L/D: 21.499965
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.057
cLalpha 0.057 cL0 0.144
cL0 0.144 cMalpha-0.066
cMalpha-0.066 cM0-0.211
cM0-0.211 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR004.txt Executable file
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FDR004
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 6.035714, Cd0: 0.009897, CL: 0.480000, CD: 0.024414, D: 9527.785965, CM: -0.601321, L/D: 18.540333
----------Cruise---------------------------------
alfa: 0.771164, Cd0: 0.005203, CL: 0.185185, CD: 0.006919, D: 6478.628035, CM: -0.259126, L/D: 26.764926
D_Wing:1155.571422, D_fuselage:3770.664809
----------Loiter---------------------------------
alfa: 3.691530, Cd0: 0.005699, CL: 0.348726, CD: 0.011851, D: 4550.243775, CM: -0.448949, L/D: 29.426995
----------Landing--------------------------------
alfa: 4.625000, Cd0: 0.009677, CL: 0.401000, CD: 0.018645, D: 9062.166794, CM: -0.509625, L/D: 21.507190
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.056
cLalpha 0.056 cL0 0.142
cL0 0.142 cMalpha-0.065
cMalpha-0.065 cM0-0.209
cM0-0.209 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR005.txt Executable file
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FDR005
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407
----------Takeoff--------------------------------
alfa: 6.035714, Cd0: 0.009897, CL: 0.480000, CD: 0.024414, D: 9527.785965, CM: -0.570214, L/D: 18.540333
----------Cruise---------------------------------
alfa: 0.771164, Cd0: 0.005203, CL: 0.185185, CD: 0.006919, D: 6478.628035, CM: -0.243812, L/D: 26.764926
D_Wing:1155.571422, D_fuselage:3770.664809
----------Loiter---------------------------------
alfa: 3.691530, Cd0: 0.005699, CL: 0.348726, CD: 0.011851, D: 4550.243775, CM: -0.424875, L/D: 29.426995
----------Landing--------------------------------
alfa: 4.625000, Cd0: 0.009677, CL: 0.401000, CD: 0.018645, D: 9062.166794, CM: -0.482750, L/D: 21.507190
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.056
cLalpha 0.056 cL0 0.142
cL0 0.142 cMalpha-0.062
cMalpha-0.062 cM0-0.196
cM0-0.196 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR006.txt Executable file
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FDR006
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 5.372164, Planform Area: 4765.305000, Wetted Area: 9841.204819
----------Takeoff--------------------------------
alfa: 5.789474, Cd0: 0.009366, CL: 0.480000, CD: 0.025911, D: 11524.531436, CM: -0.623684, L/D: 17.469300
----------Cruise---------------------------------
alfa: 0.219059, Cd0: 0.005093, CL: 0.162486, CD: 0.006598, D: 7041.632125, CM: -0.244896, L/D: 24.624973
D_Wing:1611.158629, D_fuselage:3912.112692
----------Loiter---------------------------------
alfa: 2.736511, Cd0: 0.005543, CL: 0.305981, CD: 0.010941, D: 4787.724124, CM: -0.416083, L/D: 27.967359
----------Landing--------------------------------
alfa: 4.403509, Cd0: 0.009162, CL: 0.401000, CD: 0.019382, D: 10736.626548, CM: -0.529439, L/D: 20.688886
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.057
cLalpha 0.057 cL0 0.15
cL0 0.15 cMalpha-0.068
cMalpha-0.068 cM0 -0.23
cM0 -0.23 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR007.txt Executable file
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FDR007
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 5.961418, Planform Area: 4294.280000, Wetted Area: 8871.044819
----------Takeoff--------------------------------
alfa: 5.689655, Cd0: 0.009789, CL: 0.480000, CD: 0.024698, D: 9899.382825, CM: -0.646655, L/D: 18.326955
----------Cruise---------------------------------
alfa: 0.522568, Cd0: 0.005184, CL: 0.180309, CD: 0.006854, D: 6591.510141, CM: -0.274625, L/D: 26.306567
D_Wing:1275.276731, D_fuselage:3770.664809
----------Loiter---------------------------------
alfa: 3.267986, Cd0: 0.005670, CL: 0.339543, CD: 0.011659, D: 4597.941876, CM: -0.472295, L/D: 29.121725
----------Landing--------------------------------
alfa: 4.327586, Cd0: 0.009572, CL: 0.401000, CD: 0.018782, D: 9375.811144, CM: -0.548586, L/D: 21.349896
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.058
cLalpha 0.058 cL0 0.15
cL0 0.15 cMalpha-0.072
cMalpha-0.072 cM0-0.237
cM0-0.237 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR008.txt Executable file
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FDR008
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 5.961418, Planform Area: 4294.280000, Wetted Area: 8680.251229
----------Takeoff--------------------------------
alfa: 5.689655, Cd0: 0.009659, CL: 0.480000, CD: 0.024568, D: 9847.386405, CM: -0.646655, L/D: 18.423725
----------Cruise---------------------------------
alfa: 0.522568, Cd0: 0.005081, CL: 0.180309, CD: 0.006751, D: 6492.653630, CM: -0.274625, L/D: 26.707108
D_Wing:1275.276731, D_fuselage:3665.832878
----------Loiter---------------------------------
alfa: 3.267986, Cd0: 0.005564, CL: 0.339543, CD: 0.011554, D: 4556.282608, CM: -0.472295, L/D: 29.387993
----------Landing--------------------------------
alfa: 4.327586, Cd0: 0.009445, CL: 0.401000, CD: 0.018655, D: 9312.077689, CM: -0.548586, L/D: 21.496018
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.058
cLalpha 0.058 cL0 0.15
cL0 0.15 cMalpha-0.072
cMalpha-0.072 cM0-0.237
cM0-0.237 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR009.txt Executable file
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FDR009
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 5.478266, Planform Area: 4673.011400, Wetted Area: 9672.757115
----------Takeoff--------------------------------
alfa: 6.490566, Cd0: 0.009421, CL: 0.480000, CD: 0.025645, D: 11185.579599, CM: -0.603415, L/D: 17.650069
----------Cruise---------------------------------
alfa: 0.560293, Cd0: 0.005099, CL: 0.165696, CD: 0.006634, D: 6942.134663, CM: -0.235738, L/D: 24.977908
D_Wing:1264.133474, D_fuselage:4153.626223
----------Loiter---------------------------------
alfa: 3.321215, Cd0: 0.005554, CL: 0.312024, CD: 0.011058, D: 4745.180987, CM: -0.406915, L/D: 28.218102
----------Landing--------------------------------
alfa: 5.000000, Cd0: 0.009216, CL: 0.401000, CD: 0.019238, D: 10450.457803, CM: -0.511000, L/D: 20.843746
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.053
cLalpha 0.053 cL0 0.136
cL0 0.136 cMalpha-0.062
cMalpha-0.062 cM0-0.201
cM0-0.201 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

42
ronald-plus/Ronaldplus Outputs/FDR010.txt Executable file
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FDR010
Outputs--------------------------------------------------
Wingspan: 160.020000, AR: 4.351054, Planform Area: 5885.103300, Wetted Area: 12255.124748
----------Takeoff--------------------------------
alfa: 5.961538, Cd0: 0.008588, CL: 0.480000, CD: 0.029016, D: 15938.254235, CM: -0.569846, L/D: 15.599885
----------Cruise---------------------------------
alfa: -0.739058, Cd0: 0.004911, CL: 0.131569, CD: 0.006130, D: 8078.320210, CM: -0.194613, L/D: 21.464858
D_Wing:1785.236663, D_fuselage:4837.811550
----------Loiter---------------------------------
alfa: 1.495386, Cd0: 0.005295, CL: 0.247760, CD: 0.009664, D: 5222.865680, CM: -0.319742, L/D: 25.637267
----------Landing--------------------------------
alfa: 4.442308, Cd0: 0.008409, CL: 0.401000, CD: 0.021028, D: 14385.111589, CM: -0.484769, L/D: 19.070194
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.052
cLalpha 0.052 cL0 0.17
cL0 0.17 cMalpha-0.056
cMalpha-0.056 cM0-0.236
cM0-0.236 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003

47
ronald-plus/Ronaldplus Outputs/FDR020.txt Executable file
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FDR020
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 4.929075, Planform Area: 5193.672700, Wetted Area: 10834.744604
----------Takeoff--------------------------------
alfa: 10.689189, Cd0: 0.009040, CL: 0.480000, CD: 0.027072, D: 13123.396794, CM: -0.033693, L/D: 16.720004
----------Cruise---------------------------------
alfa: 1.745533, Cd0: 0.005030, CL: 0.149085, CD: 0.006411, D: 7456.834503, CM: -0.036376, L/D: 23.253835
D_Wing:1310.651767, D_fuselage:4652.919001
----------Loiter---------------------------------
alfa: 5.303897, Cd0: 0.005450, CL: 0.280744, CD: 0.010403, D: 4961.487808, CM: -0.035309, L/D: 26.987872
----------Landing--------------------------------
alfa: 8.554054, Cd0: 0.008847, CL: 0.401000, CD: 0.019986, D: 12066.388294, CM: -0.034334, L/D: 20.063723
Inputs--------------------------------------------------
laminarflow_to 0.35 laminarflow_cruise 0.5
laminarflow_cruise 0.5 laminarflow_loiter 0.5
laminarflow_loiter 0.5 laminarflow_landing 0.35
laminarflow_landing 0.35 M_cruise 0.8
M_cruise 0.8 M_to 0.2509
M_to 0.2509 M_loiter 0.3
M_loiter 0.3 M_landing 0.28
M_landing 0.28 cLalpha 0.037
cLalpha 0.037 cL0 0.0845
cL0 0.0845 cMalpha 0.0003
cMalpha 0.0003 cM0-0.0369
cM0-0.0369 efficiency_to 0.7781
efficiency_to 0.7781 efficiency_cruise 0.98
efficiency_cruise 0.98 efficiency_loiter 0.9692
efficiency_loiter 0.9692 efficiency_landing 0.8791
efficiency_landing 0.8791 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise 173400
weight_cruise 173400 weight_to 173400
weight_to 173400 weight_loiter 133900
weight_loiter 133900 weight_landing 133900
weight_landing 133900 cd_correction 0
cd_correction 0 c_f 0.003
c_f 0.003 D_engine 240.5
D_engine 240.5 fuse_width 57.96
fuse_width 57.96 Dragredux_BLI 5.7
Dragredux_BLI 5.7 sfront_landinggear 33.7
sfront_landinggear 33.7 cd_landinggear 0.4