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