1ONERA M6 Wing. Low Mach, Inviscid 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         101353.     N/m2         14.7000     lbf/in2
 Static temperature      255.556     K            460.000     R
 Static density*         1.38207     kg/m3       0.268167E-02 slug/ft3
 Total pressure*         107883.     N/m2         15.6471     lbf/in2
 Total temperature*      260.156     K            468.280     R
 Total density*          1.44511     kg/m3       0.280398E-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        6385.23     N/m2        0.926100     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:  0.00000E+00 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   2 (*UNTITLED*), 
 J=  1: area is  7.833314E+01 in2,  5.053740E-02 m2
    Ax =  0.748534E+01 in2, Ay =  0.764344E+02 in2, Az =  0.406728E+01 in2
    Ax+=  0.374267E+01 in2, Ay+=  0.000000E+00 in2, Az+=  0.316183E+01 in2
    Ax-=  0.374267E+01 in2, Ay-=  0.764344E+02 in2, Az-=  0.905448E+00 in2
 

 Reference dynamic pressure:  9.26100E-01 lbf/in2

 Coefficients:
    Pressure            Viscous             Total
    CL  = -7.51048E-02  CL  =  0.00000E+00  CL  = -7.51048E-02
    CD  =  1.35561E-05  CD  =  0.00000E+00  CD  =  1.35561E-05
    CX  =  1.35561E-05  CX  =  0.00000E+00  CX  =  1.35561E-05
    CY  = -7.51048E-02  CY  =  0.00000E+00  CY  = -7.51048E-02
    CZ  =  1.47290E-03  CZ  =  0.00000E+00  CZ  =  1.47290E-03
    CMX =  3.39800E-02  CMX =  0.00000E+00  CMX =  3.39800E-02
    CMY = -1.12563E-03  CMY =  0.00000E+00  CMY = -1.12563E-03
    CMZ = -3.18147E-02  CMZ =  0.00000E+00  CMZ = -3.18147E-02
 
 Dimensional surface totals:
    Lift      = -1.00159E+01 lbf
    Drag      =  1.80782E-03 lbf
    X-force   =  1.80782E-03 lbf
    Y-force   = -1.00159E+01 lbf
    Z-force   =  1.96423E-01 lbf
    X-moment  =  5.43781E+01 in*lbf
    Y-moment  = -1.80135E+00 in*lbf
    Z-moment  = -5.09131E+01 in*lbf

 Subset  1 of ZONE   3 (*UNTITLED*), 
 J=  1: area is  7.833306E+01 in2,  5.053736E-02 m2
 
    Ax =  0.748535E+01 in2, Ay =  0.764346E+02 in2, Az =  0.406728E+01 in2
    Ax+=  0.374267E+01 in2, Ay+=  0.764346E+02 in2, Az+=  0.316183E+01 in2
    Ax-=  0.374267E+01 in2, Ay-=  0.000000E+00 in2, Az-=  0.905449E+00 in2
 

 Reference dynamic pressure:  9.26100E-01 lbf/in2

 Coefficients:
    Pressure            Viscous             Total
    CL  =  7.51014E-02  CL  =  0.00000E+00  CL  =  7.51014E-02
    CD  =  1.33403E-05  CD  =  0.00000E+00  CD  =  1.33403E-05
    CX  =  1.33403E-05  CX  =  0.00000E+00  CX  =  1.33403E-05
    CY  =  7.51014E-02  CY  =  0.00000E+00  CY  =  7.51014E-02
    CZ  =  1.47125E-03  CZ  =  0.00000E+00  CZ  =  1.47125E-03
    CMX = -3.39778E-02  CMX =  0.00000E+00  CMX = -3.39778E-02
    CMY = -1.12443E-03  CMY =  0.00000E+00  CMY = -1.12443E-03
    CMZ =  3.18125E-02  CMZ =  0.00000E+00  CMZ =  3.18125E-02
 
 Dimensional surface totals:
    Lift      =  1.00154E+01 lbf
    Drag      =  1.77904E-03 lbf
    X-force   =  1.77904E-03 lbf
    Y-force   =  1.00154E+01 lbf
    Z-force   =  1.96203E-01 lbf
    X-moment  = -5.43747E+01 in*lbf
    Y-moment  = -1.79943E+00 in*lbf
    Z-moment  =  5.09096E+01 in*lbf


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

 ** Total Wetted area is 1.566662E+02 in2, 1.010748E-01 m2

 Coefficients:
    Pressure            Viscous             Total
    CL  = -3.39001E-06  CL  =  0.00000E+00  CL  = -3.39001E-06
    CD  =  2.68964E-05  CD  =  0.00000E+00  CD  =  2.68964E-05
    CX  =  2.68964E-05  CX  =  0.00000E+00  CX  =  2.68964E-05
    CY  = -3.39001E-06  CY  =  0.00000E+00  CY  = -3.39001E-06
    CZ  =  2.94415E-03  CZ  =  0.00000E+00  CZ  =  2.94415E-03
    CMX =  2.13087E-06  CMX =  0.00000E+00  CMX =  2.13087E-06
    CMY = -2.25007E-03  CMY =  0.00000E+00  CMY = -2.25007E-03
    CMZ = -2.16067E-06  CMZ =  0.00000E+00  CMZ = -2.16067E-06
  
 Dimensional surface totals:
    Lift      = -4.52087E-04 lbf
    Drag      =  3.58686E-03 lbf
    X-force   =  3.58686E-03 lbf
    Y-force   = -4.52087E-04 lbf
    Z-force   =  3.92626E-01 lbf
    X-moment  =  3.41003E-03 in*lbf
    Y-moment  = -3.60078E+00 in*lbf
    Z-moment  = -3.45772E-03 in*lbf
