000			00466pam a2200145a 44500
082			_aNASA _bTN D-7635
100			_aSchmidt,James F
245	1		_aDIFFERENTIAL ANALYSIS FOR THE TURBULENT BOUNDARY LAYER ON A COMPRESSOR BLADE ELENMENT (INCLUDING BOUNDARY-LAYYER SEPARATION)
260			_a _bNasa, Washington, D.C. _c1974
300			_a28
500			_aBoundary With Nasa Tn D-7631-34,7636-40.
700			_aTodd,Carroll A
964			_gCIRC
997			_aTR12544 C
999			_c396637 _d396637