reorganize file structure
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42
ronald-plus/Ronaldplus Outputs/FDR006.txt
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42
ronald-plus/Ronaldplus Outputs/FDR006.txt
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FDR006
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Outputs--------------------------------------------------
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Wingspan: 160.000000, AR: 5.372164, Planform Area: 4765.305000, Wetted Area: 9841.204819
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----------Takeoff--------------------------------
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alfa: 5.789474, Cd0: 0.009366, CL: 0.480000, CD: 0.025911, D: 11524.531436, CM: -0.623684, L/D: 17.469300
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----------Cruise---------------------------------
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alfa: 0.219059, Cd0: 0.005093, CL: 0.162486, CD: 0.006598, D: 7041.632125, CM: -0.244896, L/D: 24.624973
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D_Wing:1611.158629, D_fuselage:3912.112692
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----------Loiter---------------------------------
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alfa: 2.736511, Cd0: 0.005543, CL: 0.305981, CD: 0.010941, D: 4787.724124, CM: -0.416083, L/D: 27.967359
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----------Landing--------------------------------
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alfa: 4.403509, Cd0: 0.009162, CL: 0.401000, CD: 0.019382, D: 10736.626548, CM: -0.529439, L/D: 20.688886
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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 0.15
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cL0 0.15 cMalpha-0.068
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cMalpha-0.068 cM0 -0.23
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cM0 -0.23 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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