000 00835pam a2200229a 44500
003 OSt
040 _cIIT Kanpur
041 _aeng
110 _aWashington. National Aeronautics and Space Administration (NASA)
245 1 _aNASA Technical Note [NASA TN D-3447]: Measured and calculated flow conditions on the forward fuselage of the X-15 airplane and model at mach numbers from 3.0 to 8.0
_cMurray Palitz
260 _bNASA
_c1966
_aWashington
300 _a44p
440 _aNational Aeronautics and Space Administration
440 _aNASA Technical Note
500 _aBound together NASA TN D-3441 to 3450
500 _aBound vol. Acc. No. 64324 contains Acc. No. TR8886 to TR8894
650 _aAeronautics
650 _aAircraft
650 _aFlight and wind-tunnel tests
700 _aPalitz, Murray
942 _cBK
999 _c393824
_d393824