000			00483pam a2200145a 44500
082			_aNASA _bCR-2068
100			_aHerring,H J
245	1		_aCOMPUTER PROGRAM FOR CALCULATING LAMINAR AND TURBULENT BOUNDARY LAYER DEVELOPMENT IN COMPRESSIBLE FLOW.
260			_a _bNational Aeronautics And Space Administration, Washington, D.C. _c1972
300			_a87
500			_aBound With Nasa Cr-2065,2069-70 Lack No 2066-67
700			_aMellor,G L
964			_gCIRC
997			_aTR11277 C
999			_c395793 _d395793