1RAE 2822, Two-Dimensional Transonic Turbulent Flow
 M_infty = 0.729, alpha = 2.31 deg.
 
 Freestream conditions (* indicates calculated)
 
 Mach number                   0.729
 Angle of attack               2.310 degrees
 Yaw angle                     0.000 degrees
 Gamma                         1.400
 Gas constant (R)            286.959 m2/s2-K         1716.000 ft2/s2-R
 Static pressure         108988.     N/m2         15.8073     lbf/in2
 Static temperature      255.556     K            460.000     R
 Static density*         1.48618     kg/m3       0.288367E-02 slug/ft3
 Total pressure*         155209.     N/m2         22.5112     lbf/in2
 Total temperature*      282.718     K            508.893     R
 Total density*          1.91313     kg/m3       0.371208E-02 slug/ft3
 Speed of sound          320.418     m/s          1051.24     ft/s
 Velocity                233.585     m/s          766.353     ft/s
 Dynamic pressure        40544.4     N/m2         5.88047     lbf/in2
 Laminar Viscosity      0.162748E-04 kg/m-s      0.339906E-06 slug/ft-s
 Reynolds Number*       0.213305E+08 1/m         0.650154E+07 1/ft
 Enthalpy*               256669.     m2/s2       0.276276E+07 ft2/s2
 Stagnation Enthalpy*    283950.     m2/s2       0.305641E+07 ft2/s2



 Downstream axis is +X, vertical axis is +Y

 Reference area  :  1.00000E+00 ft2

 Reference length:  1.00000E+00 ft      

 Moments computed about reference point:
                X:  2.50000E-01 ft      
                Y:  0.00000E+00 ft      
                Z:  0.00000E+00 ft      

 Force integration modes: 

 Integrate only over points with zero velocity

 Normal derivatives computed second order

 Pressure integration performed as (p-pinf)*dA
1Subset  1 of ZONE   1 (*UNTITLED*), 
 J=  1: area is  2.926783E+02 in2,  1.888243E-01 m2
    Ax =  0.355051E+02 in2, Ay =  0.288000E+03 in2, Az =  0.000000E+00 in2
    Ax+=  0.177526E+02 in2, Ay+=  0.144000E+03 in2, Az+=  0.000000E+00 in2
    Ax-=  0.177526E+02 in2, Ay-=  0.144000E+03 in2, Az-=  0.000000E+00 in2
 

 Reference dynamic pressure:  5.88047E+00 lbf/in2

 Coefficients:
    Pressure            Viscous             Total
    CL  =  7.30925E-01  CL  = -1.01002E-06  CL  =  7.30924E-01
    CD  =  6.20041E-03  CD  =  2.50384E-05  CD  =  6.22545E-03
    CX  = -2.32654E-02  CX  =  2.50588E-05  CX  = -2.32404E-02
    CY  =  7.30581E-01  CY  =  0.00000E+00  CY  =  7.30581E-01
    CZ  =  0.00000E+00  CZ  =  0.00000E+00  CZ  =  0.00000E+00
    CMX =  0.00000E+00  CMX =  0.00000E+00  CMX =  0.00000E+00
    CMY =  0.00000E+00  CMY =  0.00000E+00  CMY =  0.00000E+00
    CMZ =  9.01768E-02  CMZ = -1.31947E-07  CMZ =  9.01766E-02
 
 First order viscous coefficients:
    CX  =  2.50588E-05   0.00000E+00 percent difference
    CY  =  0.00000E+00   0.00000E+00 percent difference
    CZ  =  0.00000E+00   0.00000E+00 percent difference
 
 Dimensional surface totals:
    Lift      =  6.18938E+02 lbf
    Drag      =  5.27163E+00 lbf
    X-force   = -1.96797E+01 lbf
    Y-force   =  6.18647E+02 lbf
    Z-force   =  0.00000E+00 lbf
    X-moment  =  0.00000E+00 in*lbf
    Y-moment  =  0.00000E+00 in*lbf
    Z-moment  =  9.16325E+02 in*lbf
    Heat xfer =  0.00000E+00 ft*lbf/sec
              =  0.00000E+00 Btu/hr
              =  0.00000E+00 Btu/sec
              =  0.00000E+00 Watts


 *********************************** Totals ***********************************

 ** Total Wetted area is 2.926783E+02 in2, 1.888243E-01 m2

 Coefficients:
    Pressure            Viscous             Total
    CL  =  7.30925E-01  CL  = -1.01002E-06  CL  =  7.30924E-01
    CD  =  6.20041E-03  CD  =  2.50384E-05  CD  =  6.22545E-03
    CX  = -2.32654E-02  CX  =  2.50588E-05  CX  = -2.32404E-02
    CY  =  7.30581E-01  CY  =  0.00000E+00  CY  =  7.30581E-01
    CZ  =  0.00000E+00  CZ  =  0.00000E+00  CZ  =  0.00000E+00
    CMX =  0.00000E+00  CMX =  0.00000E+00  CMX =  0.00000E+00
    CMY =  0.00000E+00  CMY =  0.00000E+00  CMY =  0.00000E+00
    CMZ =  9.01768E-02  CMZ = -1.31947E-07  CMZ =  9.01766E-02
  
 Dimensional surface totals:
    Lift      =  6.18938E+02 lbf
    Drag      =  5.27163E+00 lbf
    X-force   = -1.96797E+01 lbf
    Y-force   =  6.18647E+02 lbf
    Z-force   =  0.00000E+00 lbf
    X-moment  =  0.00000E+00 in*lbf
    Y-moment  =  0.00000E+00 in*lbf
    Z-moment  =  9.16325E+02 in*lbf
    Heat xfer =  0.00000E+00 ft*lbf/sec
              =  0.00000E+00 Btu/hr
              =  0.00000E+00 Btu/sec
              =  0.00000E+00 Watts
