Total_Forces.txt

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 Vortex Lattice Output -- Total Forces

 Configuration: Boeing X-48B                                                
     # Surfaces =   4
     # Strips   =  50
     # Vortices = 500

  Sref =  9.3500       Cref =  1.4600       Bref =  6.4000    
  Xref =  0.0000       Yref =  0.0000       Zref =  0.0000    

 Standard axis orientation,  X fwd, Z down         

 Run case:  -unnamed-                              

  Alpha =   0.08028     pb/2V =  -0.00000     p'b/2V =  -0.00000
  Beta  =   0.00000     qc/2V =   0.00000
  Mach  =     0.000     rb/2V =  -0.00000     r'b/2V =  -0.00000

  CXtot =  -0.00081     Cltot =  -0.00000     Cl'tot =  -0.00000
  CYtot =   0.00000     Cmtot =  -0.14552
  CZtot =  -0.10981     Cntot =  -0.00000     Cn'tot =  -0.00000

  CLtot =   0.10980
  CDtot =   0.00096
  CDvis =   0.00000     CDind = 0.0009602
  CLff  =   0.10979     CDff  = 0.0009684    | Trefftz
  CYff  =   0.00000         e =    0.9044    | Plane  

   Elevon1         =   0.00000
   Elevon2         =   0.00000
   Elevon3         =   0.00000
   Aileron1        =   0.00000
   Aileron2        =   0.00000

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