1ONERA M6 Wing. Transonic Turbulent Flow. M_infty=0.84, alpha=3.06 deg. Rec=11.72E+06. Freestream conditions (* indicates calculated) Mach number 0.840 Angle of attack 3.060 degrees Yaw angle 0.000 degrees Gamma 1.400 Gas constant (R) 286.959 m2/s2-K 1716.000 ft2/s2-R Static pressure 315980. N/m2 45.8290 lbf/in2 Static temperature 255.556 K 460.000 R Static density* 4.30878 kg/m3 0.836041E-02 slug/ft3 Total pressure* 501297. N/m2 72.7070 lbf/in2 Total temperature* 291.577 K 524.838 R Total density* 5.99132 kg/m3 0.116251E-01 slug/ft3 Speed of sound 320.418 m/s 1051.24 ft/s Velocity 268.991 m/s 882.515 ft/s Dynamic pressure 155883. N/m2 22.6089 lbf/in2 Laminar Viscosity 0.162748E-04 kg/m-s 0.339906E-06 slug/ft-s Reynolds Number* 0.712157E+08 1/m 0.217065E+08 1/ft Enthalpy* 256669. m2/s2 0.276276E+07 ft2/s2 Stagnation Enthalpy* 292847. m2/s2 0.315218E+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 only over points with zero velocity Normal derivatives computed second order Pressure integration performed as (p-pinf)*dA ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** 4 of 2409 points have too much stretching for second order derivatives. First order derivatives used instead. ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** 1Subset 1 of ZONE 2 (*UNTITLED*), J= 1: area is 7.833311E+01 in2, 5.053739E-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: 2.26089E+01 lbf/in2 y+ values: Average (one point off) = 2.42377E+01 Average (two points off) = 5.38232E+01 Maximum (one point off) = 3.78068E+01 at I= 18, J= 1, K= 1 where (two points) = 8.36043E+01 Heat transfer values: Maximum = 1.53565E+17 at I= 1, J= 1, K= 33 Integrated (2nd order) = 5.39194E+11 Integrated (1st order) = -3.46360E+10 Coefficients: Pressure Viscous Total CL = -5.67242E-02 CL = -9.78358E-05 CL = -5.68221E-02 CD = 3.87602E-03 CD = 1.48161E-03 CD = 5.35763E-03 CX = 6.89853E-03 CX = 1.48472E-03 CX = 8.38325E-03 CY = -5.64364E-02 CY = -1.86053E-05 CY = -5.64550E-02 CZ = -1.54675E-03 CZ = 2.37374E-05 CZ = -1.52301E-03 CMX = 2.81395E-02 CMX = 4.98850E-06 CMX = 2.81445E-02 CMY = 2.09020E-03 CMY = 6.80402E-04 CMY = 2.77060E-03 CMZ = -2.82214E-02 CMZ = 4.54883E-05 CMZ = -2.81759E-02 First order viscous coefficients: CX = 1.48472E-03 -1.56818E-05 percent difference CY = -1.86053E-05 -1.17321E-04 percent difference CZ = 2.37377E-05 1.41765E-03 percent difference Dimensional surface totals: Lift = -1.84995E+02 lbf Drag = 1.74428E+01 lbf X-force = 2.72932E+01 lbf Y-force = -1.83800E+02 lbf Z-force = -4.95845E+00 lbf X-moment = 1.09955E+03 in*lbf Y-moment = 1.08242E+02 in*lbf Z-moment = -1.10078E+03 in*lbf Heat xfer = 3.69465E+10 ft*lbf/sec = 1.70915E+11 Btu/hr = 4.74763E+07 Btu/sec = 5.00927E+10 Watts ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** 1 of 2409 points are in a left-handed coordinate system. Please check the ordering of your SUBSETS. ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** 1 of 2409 points are in a left-handed coordinate system. Please check the ordering of your SUBSETS. ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** 4 of 2409 points have too much stretching for second order derivatives. First order derivatives used instead. ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** ** WARNING **** WARNING **** WARNING **** WARNING **** WARNING **** WARNING ** 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: 2.26089E+01 lbf/in2 y+ values: Average (one point off) = 2.09416E+01 Average (two points off) = 4.65221E+01 Maximum (one point off) = 3.70544E+01 at I= 7, J= 1, K= 1 where (two points) = 8.30014E+01 Heat transfer values: Maximum = -1.02355E+18 at I= 73, J= 1, K= 33 Integrated (2nd order) = -3.59388E+12 Integrated (1st order) = 1.74624E+12 Coefficients: Pressure Viscous Total CL = 1.97770E-01 CL = 2.08819E-05 CL = 1.97791E-01 CD = 2.08153E-03 CD = 1.33882E-03 CD = 3.42035E-03 CX = -8.47874E-03 CX = 1.33580E-03 CX = -7.14294E-03 CY = 1.97599E-01 CY = 9.23208E-05 CY = 1.97692E-01 CZ = 9.16766E-03 CZ = -4.16807E-05 CZ = 9.12597E-03 CMX = -9.04356E-02 CMX = -4.88842E-05 CMX = -9.04845E-02 CMY = -9.57462E-03 CMY = 6.10764E-04 CMY = -8.96386E-03 CMZ = 8.17317E-02 CMZ = -1.00413E-05 CMZ = 8.17217E-02 First order viscous coefficients: CX = 1.33580E-03 -3.48601E-05 percent difference CY = 9.23208E-05 -2.36435E-05 percent difference CZ = -4.16806E-05 -6.98257E-05 percent difference Dimensional surface totals: Lift = 6.43945E+02 lbf Drag = 1.11356E+01 lbf X-force = -2.32552E+01 lbf Y-force = 6.43621E+02 lbf Z-force = 2.97113E+01 lbf X-moment = -3.53507E+03 in*lbf Y-moment = -3.50202E+02 in*lbf Z-moment = 3.19272E+03 in*lbf Heat xfer = -2.46259E+11 ft*lbf/sec = -1.13920E+12 Btu/hr = -3.16443E+08 Btu/sec = -3.33883E+11 Watts *********************************** Totals *********************************** ** Total Wetted area is 1.566662E+02 in2, 1.010747E-01 m2 Coefficients: Pressure Viscous Total CL = 1.41046E-01 CL = -7.69538E-05 CL = 1.40969E-01 CD = 5.95755E-03 CD = 2.82044E-03 CD = 8.77798E-03 CX = -1.58022E-03 CX = 2.82052E-03 CX = 1.24031E-03 CY = 1.41163E-01 CY = 7.37155E-05 CY = 1.41237E-01 CZ = 7.62090E-03 CZ = -1.79433E-05 CZ = 7.60296E-03 CMX = -6.22961E-02 CMX = -4.38957E-05 CMX = -6.23400E-02 CMY = -7.48443E-03 CMY = 1.29117E-03 CMY = -6.19326E-03 CMZ = 5.35104E-02 CMZ = 3.54470E-05 CMZ = 5.35458E-02 Dimensional surface totals: Lift = 4.58950E+02 lbf Drag = 2.85783E+01 lbf X-force = 4.03804E+00 lbf Y-force = 4.59822E+02 lbf Z-force = 2.47528E+01 lbf X-moment = -2.43551E+03 in*lbf Y-moment = -2.41960E+02 in*lbf Z-moment = 2.09194E+03 in*lbf Heat xfer = -2.09313E+11 ft*lbf/sec = -9.68281E+11 Btu/hr = -2.68967E+08 Btu/sec = -2.83790E+11 Watts