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senior-design/ronald-plus/Ronaldplus Outputs/FDR001.txt
2010-04-17 12:00:00 -05:00

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