reorganize file structure
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ronald-plus/Ronaldplus Outputs/FDR010.txt
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42
ronald-plus/Ronaldplus Outputs/FDR010.txt
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FDR010
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Outputs--------------------------------------------------
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Wingspan: 160.020000, AR: 4.351054, Planform Area: 5885.103300, Wetted Area: 12255.124748
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----------Takeoff--------------------------------
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alfa: 5.961538, Cd0: 0.008588, CL: 0.480000, CD: 0.029016, D: 15938.254235, CM: -0.569846, L/D: 15.599885
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----------Cruise---------------------------------
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alfa: -0.739058, Cd0: 0.004911, CL: 0.131569, CD: 0.006130, D: 8078.320210, CM: -0.194613, L/D: 21.464858
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D_Wing:1785.236663, D_fuselage:4837.811550
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----------Loiter---------------------------------
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alfa: 1.495386, Cd0: 0.005295, CL: 0.247760, CD: 0.009664, D: 5222.865680, CM: -0.319742, L/D: 25.637267
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----------Landing--------------------------------
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alfa: 4.442308, Cd0: 0.008409, CL: 0.401000, CD: 0.021028, D: 14385.111589, CM: -0.484769, L/D: 19.070194
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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 0.052
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cLalpha 0.052 cL0 0.17
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cL0 0.17 cMalpha-0.056
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cMalpha-0.056 cM0-0.236
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cM0-0.236 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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