1RAE 2822, Two-Dimensional Inviscid, Low-Mach Flow.
 M_infty = 0.3, alpha = 0.0 deg.
 
 Freestream conditions (* indicates calculated)
 
 Mach number                   0.300
 Angle of attack               0.000 degrees
 Yaw angle                     0.000 degrees
 Gamma                         1.400
 Gas constant (R)            286.959 m2/s2-K         1716.000 ft2/s2-R
 Static pressure         96526.6     N/m2         14.0000     lbf/in2
 Static temperature      255.556     K            460.000     R
 Static density*         1.31626     kg/m3       0.255397E-02 slug/ft3
 Total pressure*         102746.     N/m2         14.9020     lbf/in2
 Total temperature*      260.156     K            468.280     R
 Total density*          1.37629     kg/m3       0.267045E-02 slug/ft3
 Speed of sound          320.418     m/s          1051.24     ft/s
 Velocity                96.1253     m/s          315.372     ft/s
 Dynamic pressure        6081.18     N/m2        0.882000     lbf/in2
 Laminar Viscosity      0.162748E-04 kg/m-s      0.339906E-06 slug/ft-s
 Enthalpy*               256669.     m2/s2       0.276276E+07 ft2/s2
 Stagnation Enthalpy*    261289.     m2/s2       0.281249E+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 over all selected points

 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:  8.82000E-01 lbf/in2

 Coefficients:
    Pressure            Viscous             Total
    CL  =  2.77441E-01  CL  =  0.00000E+00  CL  =  2.77441E-01
    CD  =  2.96066E-04  CD  =  0.00000E+00  CD  =  2.96066E-04
    CX  =  2.96066E-04  CX  =  0.00000E+00  CX  =  2.96066E-04
    CY  =  2.77441E-01  CY  =  0.00000E+00  CY  =  2.77441E-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 =  8.29890E-02  CMZ =  0.00000E+00  CMZ =  8.29890E-02
 
 Dimensional surface totals:
    Lift      =  3.52372E+01 lbf
    Drag      =  3.76028E-02 lbf
    X-force   =  3.76028E-02 lbf
    Y-force   =  3.52372E+01 lbf
    Z-force   =  0.00000E+00 lbf
    X-moment  =  0.00000E+00 in*lbf
    Y-moment  =  0.00000E+00 in*lbf
    Z-moment  =  1.26483E+02 in*lbf


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

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

 Coefficients:
    Pressure            Viscous             Total
    CL  =  2.77441E-01  CL  =  0.00000E+00  CL  =  2.77441E-01
    CD  =  2.96066E-04  CD  =  0.00000E+00  CD  =  2.96066E-04
    CX  =  2.96066E-04  CX  =  0.00000E+00  CX  =  2.96066E-04
    CY  =  2.77441E-01  CY  =  0.00000E+00  CY  =  2.77441E-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 =  8.29890E-02  CMZ =  0.00000E+00  CMZ =  8.29890E-02
  
 Dimensional surface totals:
    Lift      =  3.52372E+01 lbf
    Drag      =  3.76028E-02 lbf
    X-force   =  3.76028E-02 lbf
    Y-force   =  3.52372E+01 lbf
    Z-force   =  0.00000E+00 lbf
    X-moment  =  0.00000E+00 in*lbf
    Y-moment  =  0.00000E+00 in*lbf
    Z-moment  =  1.26483E+02 in*lbf
