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2010-04-17 12:00:00 -05:00

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Executable File

FDR006
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 5.372164, Planform Area: 4765.305000, Wetted Area: 9841.204819
----------Takeoff--------------------------------
alfa: 5.789474, Cd0: 0.009366, CL: 0.480000, CD: 0.025911, D: 11524.531436, CM: -0.623684, L/D: 17.469300
----------Cruise---------------------------------
alfa: 0.219059, Cd0: 0.005093, CL: 0.162486, CD: 0.006598, D: 7041.632125, CM: -0.244896, L/D: 24.624973
D_Wing:1611.158629, D_fuselage:3912.112692
----------Loiter---------------------------------
alfa: 2.736511, Cd0: 0.005543, CL: 0.305981, CD: 0.010941, D: 4787.724124, CM: -0.416083, L/D: 27.967359
----------Landing--------------------------------
alfa: 4.403509, Cd0: 0.009162, CL: 0.401000, CD: 0.019382, D: 10736.626548, CM: -0.529439, L/D: 20.688886
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 0.057
cLalpha 0.057 cL0 0.15
cL0 0.15 cMalpha-0.068
cMalpha-0.068 cM0 -0.23
cM0 -0.23 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