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