000			00510pam a2200145a 44500
082			_aNASA _bTR R-84
100			_aPetterson,Elizabeth W
245	1		_aORDINATES AND THEORETICAL PRESSURE-DISTRIBUTION DATA FOR NACA 6- AND 6A-SERIES AIRFOIL SECTIONS WITH THICKNESSES FROM 2 TO 21 AND FROM 2 TO 15 PERCENT CHORD, RESPECTIVELY
260			_a _bNasa, Washington, D.C. _c1961
300			_a86
500			_aBound With Nasa Tr R-81-83,85-90
700			_aBraslow,Albert L
964			_gCIRC
997			_aTR14357 C
999			_c398972 _d398972