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