WingPlanAnal

     Wing Planform Geometry Analysis
     Virginia Tech Aircraft Design Software Series
     W.H. Mason, Department of Aerospace and Ocean Engineering
     Virginia Tech, Blacksburg, VA 24061, email: whmason@vt.edu
     version: January 22, 2006

     Planform Properties
 Enter name of data set:
B2Plan.inp

     Input Case Title:  B-2 Planform                                               

     Planform Points

     Leading Edge     iLM =  2

       i        YLE            XLE
       1        0.0000        0.0000
       2       86.0000       59.4700

     Trailing Edge     iTM =  6

       i        YTE            XTE
       1        0.0000       65.4600
       2       12.6600       56.8200
       3       22.5000       63.2400
       4       43.9000       48.2600
       5       72.7400       67.9000
       6       86.0000       59.4700

     Interpolated LE and TE points and sweep

   i        eta        y       XLE  LE sweep(deg)  XTE  TE sweep(deg)
   0       0.000     0.000     0.000    34.664    65.460   -34.312
   1       0.050     4.300     2.974    34.664    62.525   -34.312
   2       0.100     8.600     5.947    34.664    59.591   -34.312
   3       0.150    12.900     8.921    34.664    56.977    33.122
   4       0.200    17.200    11.894    34.664    59.782    33.122
   5       0.250    21.500    14.868    34.664    62.588    33.122
   6       0.300    25.800    17.841    34.664    60.930   -34.992
   7       0.350    30.100    20.815    34.664    57.920   -34.992
   8       0.400    34.400    23.788    34.664    54.910   -34.992
   9       0.450    38.700    26.762    34.664    51.900   -34.992
  10       0.500    43.000    29.735    34.664    48.890   -34.992
  11       0.550    47.300    32.709    34.664    50.575    34.255
  12       0.600    51.600    35.682    34.664    53.504    34.255
  13       0.650    55.900    38.656    34.664    56.432    34.255
  14       0.700    60.200    41.629    34.664    59.360    34.255
  15       0.750    64.500    44.603    34.664    62.289    34.255
  16       0.800    68.800    47.576    34.664    65.217    34.255
  17       0.850    73.100    50.550    34.664    67.671   -32.446
  18       0.900    77.400    53.523    34.664    64.937   -32.446
  19       0.950    81.700    56.497    34.664    62.204   -32.446
  20       1.000    86.000    59.470    34.664    59.470   -32.446

     Integral Quantities

     Planform Area            =  5039.31300
     Mean Aerodynamic Chord   =    39.24220
     X-Centroid               =    39.75905
     Spanwise position of MAC =    29.12163
     X-Leading Edge of MAC    =    20.13795
     Quarter Chord of MAC     =    29.94850
     Aspect Ratio             =     5.87064
     Average Chord            =    29.29833
     Taper Ratio              =     0.00000




     Do you want LE/TE and Sweep? (Y/N) 
y

     Input span location, Y= 
12.

     y   =   12.00000     eta   =    0.13953
     X-le=    8.29814     sweep =   34.66432
     X-te=   57.27042     sweep =  -34.31216
     c   =   48.97228

     Do you want another station? (Y/N) 
n
Press RETURN to quit the program.