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 |
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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 |