reorganize file structure
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ronald-plus/Ronaldplus Outputs/FDR003.txt
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42
ronald-plus/Ronaldplus Outputs/FDR003.txt
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FDR003
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Outputs--------------------------------------------------
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Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8646.272379
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----------Takeoff--------------------------------
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alfa: 5.894737, Cd0: 0.009903, CL: 0.480000, CD: 0.024420, D: 9530.278297, CM: -0.600053, L/D: 18.535485
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----------Cruise---------------------------------
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alfa: 0.722547, Cd0: 0.005208, CL: 0.185185, CD: 0.006924, D: 6483.328324, CM: -0.258688, L/D: 26.745522
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D_Wing:1159.593905, D_fuselage:3771.626725
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----------Loiter---------------------------------
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alfa: 3.591678, Cd0: 0.005704, CL: 0.348726, CD: 0.011856, D: 4552.237898, CM: -0.448051, L/D: 29.414104
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----------Landing--------------------------------
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alfa: 4.508772, Cd0: 0.009684, CL: 0.401000, CD: 0.018651, D: 9065.211714, CM: -0.508579, L/D: 21.499965
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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 0.057
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cLalpha 0.057 cL0 0.144
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cL0 0.144 cMalpha-0.066
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cMalpha-0.066 cM0-0.211
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cM0-0.211 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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