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Ronaldplus Outputs/FDR001.txt
Executable file
42
Ronaldplus Outputs/FDR001.txt
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FDR001
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Outputs--------------------------------------------------
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Wingspan: 140.000000, AR: 4.816577, Planform Area: 4069.280000, Wetted Area: 8408.002654
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----------Takeoff--------------------------------
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alfa: 6.125000, Cd0: 0.009957, CL: 0.480000, CD: 0.028410, D: 10790.513767, CM: -0.582875, L/D: 15.932485
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----------Cruise---------------------------------
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alfa: 0.951405, Cd0: 0.005179, CL: 0.190279, CD: 0.007481, D: 6817.381579, CM: -0.256939, L/D: 25.434985
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D_Wing:993.322998, D_fuselage:3770.664809
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----------Loiter---------------------------------
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alfa: 3.952095, Cd0: 0.005682, CL: 0.358317, CD: 0.013937, D: 5208.157173, CM: -0.445982, L/D: 25.709670
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----------Landing--------------------------------
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alfa: 4.714286, Cd0: 0.009735, CL: 0.401000, CD: 0.021135, D: 9997.294077, CM: -0.494000, L/D: 18.973583
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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 0.056
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cLalpha 0.056 cL0 0.137
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cL0 0.137 cMalpha-0.063
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cMalpha-0.063 cM0-0.197
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cM0-0.197 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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