000			00423pam a2200145a 44500
082			_aNASA _bCR-321
100			_aConner,F,Willey,C
245	1		_aA FLIGHT AND WIND TUNNEL INVESTIGATION OF THE EFFECT OF ANGLE-OF-ATTACK RATE ON MAXIMUM LIFT COEFFICIENT
260			_a _bNasa, Washington, D.C. _c1965
300			_a51
500			_aBound With Nasa Cr-322-24.
700			_aTwomey,W
964			_gCIRC
997			_a64883 C
999			_c448337 _d448337