000			00536pam a2200133a 44500
082			_aNASA _bMEMO 5-24-59L
100			_aBertram,Mitchel H
245	1		_aA SIMPLE METHOD FOR DETERMINING HEAT TRANSFER, SKIN FRICTION, AND BOUNDARY-LAYER THICKNESS FOR HYPERSONIC LAMINAR BOUNDARY-LAYER FLOWS IN A PRESSURE GRADIENT
260			_a _bNasa, Washington, D.C. _c1959
500			_aBound With Nasa Memo 5-12-59l-5-23-59l And 5-24-59l-5-28-59l, Lack No.14-17, 19, 21-22, 27
700			_aFeller,William V
964			_gCIRC
997			_aTR7409 C
999			_c395576 _d395576