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