FDR009
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 5.478266, Planform Area: 4673.011400, Wetted Area: 9672.757115 

----------Takeoff--------------------------------
 alfa: 6.490566, Cd0: 0.009421, CL: 0.480000, CD: 0.025645, D: 11185.579599, CM: -0.603415, L/D: 17.650069 

----------Cruise---------------------------------
 alfa: 0.560293, Cd0: 0.005099, CL: 0.165696, CD: 0.006634, D: 6942.134663,  CM: -0.235738, L/D: 24.977908 
 D_Wing:1264.133474, D_fuselage:4153.626223
----------Loiter---------------------------------
 alfa: 3.321215, Cd0: 0.005554, CL: 0.312024, CD: 0.011058, D: 4745.180987, CM: -0.406915, L/D: 28.218102 

----------Landing--------------------------------
 alfa: 5.000000, Cd0: 0.009216, CL: 0.401000, CD: 0.019238, D: 10450.457803, CM: -0.511000, L/D: 20.843746 

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 0.053 
cLalpha 0.053      cL0 0.136 
cL0 0.136      cMalpha-0.062 
cMalpha-0.062      cM0-0.201 
cM0-0.201      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