000			00461pam a2200145a 44500
082			_aNASA _bTN D-2230
100			_aPappas,C C
245	1		_aMEASUREMENT OF HEAT TRANSFER AND RECOVERY FACTOR OF A COMPRESSIBLE TURBULENT BOUNDARY LAYER ON A SHARP CONE WITH FOREIGN GAS INJECTION
260			_a _bNasa, Washington, D.C. _c1964
300			_a83
500			_aBound With Nasa Tn D-2226-2229
700			_aOkuno,Arthur F
964			_gCIRC
997			_aTR12842 C
999			_c396612 _d396612