000			00446pam a2200145a 44500
082			_aNASA _bTN D-6221 -
100			_aBeckwith,Ivan E
245	1		_aCALCULATION BY A FINITE-DIFFERENCE METHOD OF SUPERSONIC TURBULENT BOUNDARY LAYERS WITH TANGENTIAL SLOT INJECTION
260			_a _bNasa, Washington, D.C. _c1971
300			_a74
500			_aBound With Nasa Tn D-6220-29
700			_aBushnell,Dennis M
964			_gCIRC
997			_aTR9567 C
999			_c393910 _d393910