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