FDR008
Outputs--------------------------------------------------
Wingspan: 160.000000, AR: 5.961418, Planform Area: 4294.280000, Wetted Area: 8680.251229 

----------Takeoff--------------------------------
 alfa: 5.689655, Cd0: 0.009659, CL: 0.480000, CD: 0.024568, D: 9847.386405, CM: -0.646655, L/D: 18.423725 

----------Cruise---------------------------------
 alfa: 0.522568, Cd0: 0.005081, CL: 0.180309, CD: 0.006751, D: 6492.653630,  CM: -0.274625, L/D: 26.707108 
 D_Wing:1275.276731, D_fuselage:3665.832878
----------Loiter---------------------------------
 alfa: 3.267986, Cd0: 0.005564, CL: 0.339543, CD: 0.011554, D: 4556.282608, CM: -0.472295, L/D: 29.387993 

----------Landing--------------------------------
 alfa: 4.327586, Cd0: 0.009445, CL: 0.401000, CD: 0.018655, D: 9312.077689, CM: -0.548586, L/D: 21.496018 

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 0.058 
cLalpha 0.058      cL0  0.15 
cL0  0.15      cMalpha-0.072 
cMalpha-0.072      cM0-0.237 
cM0-0.237      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