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senior-design/ronald-plus/Ronaldplus Outputs/FDR010.txt
2010-04-17 12:00:00 -05:00

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FDR010
Outputs--------------------------------------------------
Wingspan: 160.020000, AR: 4.351054, Planform Area: 5885.103300, Wetted Area: 12255.124748
----------Takeoff--------------------------------
alfa: 5.961538, Cd0: 0.008588, CL: 0.480000, CD: 0.029016, D: 15938.254235, CM: -0.569846, L/D: 15.599885
----------Cruise---------------------------------
alfa: -0.739058, Cd0: 0.004911, CL: 0.131569, CD: 0.006130, D: 8078.320210, CM: -0.194613, L/D: 21.464858
D_Wing:1785.236663, D_fuselage:4837.811550
----------Loiter---------------------------------
alfa: 1.495386, Cd0: 0.005295, CL: 0.247760, CD: 0.009664, D: 5222.865680, CM: -0.319742, L/D: 25.637267
----------Landing--------------------------------
alfa: 4.442308, Cd0: 0.008409, CL: 0.401000, CD: 0.021028, D: 14385.111589, CM: -0.484769, L/D: 19.070194
Inputs--------------------------------------------------
laminarflow_to 0.4 laminarflow_cruise 0.4
laminarflow_cruise 0.4 laminarflow_loiter 0.4
laminarflow_loiter 0.4 laminarflow_landing 0.4
laminarflow_landing 0.4 M_cruise 0.8
M_cruise 0.8 M_to 0.2
M_to 0.2 M_loiter 0.3
M_loiter 0.3 M_landing 0.2
M_landing 0.2 cLalpha 0.052
cLalpha 0.052 cL0 0.17
cL0 0.17 cMalpha-0.056
cMalpha-0.056 cM0-0.236
cM0-0.236 efficiency_to 0.8
efficiency_to 0.8 efficiency_cruise 0.8
efficiency_cruise 0.8 efficiency_loiter 0.8
efficiency_loiter 0.8 efficiency_landing 0.8
efficiency_landing 0.8 alt_cruise 35000
alt_cruise 35000 alt_to 0
alt_to 0 alt_loiter 10000
alt_loiter 10000 alt_landing 0
alt_landing 0 weight_cruise160000
weight_cruise160000 weight_to160000
weight_to160000 weight_loiter130000
weight_loiter130000 weight_landing130000
weight_landing130000 cd_correction 0
cd_correction 0 c_f 0.003