reorganize file structure
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42
ronald-plus/Ronaldplus Outputs/FDR009.txt
Executable file
42
ronald-plus/Ronaldplus Outputs/FDR009.txt
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FDR009
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Outputs--------------------------------------------------
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Wingspan: 160.000000, AR: 5.478266, Planform Area: 4673.011400, Wetted Area: 9672.757115
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----------Takeoff--------------------------------
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alfa: 6.490566, Cd0: 0.009421, CL: 0.480000, CD: 0.025645, D: 11185.579599, CM: -0.603415, L/D: 17.650069
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----------Cruise---------------------------------
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alfa: 0.560293, Cd0: 0.005099, CL: 0.165696, CD: 0.006634, D: 6942.134663, CM: -0.235738, L/D: 24.977908
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D_Wing:1264.133474, D_fuselage:4153.626223
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----------Loiter---------------------------------
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alfa: 3.321215, Cd0: 0.005554, CL: 0.312024, CD: 0.011058, D: 4745.180987, CM: -0.406915, L/D: 28.218102
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----------Landing--------------------------------
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alfa: 5.000000, Cd0: 0.009216, CL: 0.401000, CD: 0.019238, D: 10450.457803, CM: -0.511000, L/D: 20.843746
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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 0.053
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cLalpha 0.053 cL0 0.136
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cL0 0.136 cMalpha-0.062
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cMalpha-0.062 cM0-0.201
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cM0-0.201 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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