FDR002
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 6.122637, Planform Area: 4181.205000, Wetted Area: 8638.340407 

----------Takeoff--------------------------------
 alfa: 5.894737, Cd0: 0.009897, CL: 0.480000, CD: 0.024414, D: 9527.785965, CM: -0.600053, L/D: 18.540333 

----------Cruise---------------------------------
 alfa: 0.722547, Cd0: 0.005203, CL: 0.185185, CD: 0.006919, D: 6478.628035,  CM: -0.258688, L/D: 26.764926 
 D_Wing:1155.571422, D_fuselage:3770.664809
----------Loiter---------------------------------
 alfa: 3.591678, Cd0: 0.005699, CL: 0.348726, CD: 0.011851, D: 4550.243775, CM: -0.448051, L/D: 29.426995 

----------Landing--------------------------------
 alfa: 4.508772, Cd0: 0.009677, CL: 0.401000, CD: 0.018645, D: 9062.166794, CM: -0.508579, L/D: 21.507190 

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 0.144 
cL0 0.144      cMalpha-0.066 
cMalpha-0.066      cM0-0.211 
cM0-0.211      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