000			00525pam a2200145a 44500
082			_aNASA _bMEMO 5-16-59A
100			_aLopez,Armando E,Buell,Donald A
245	1		_aTHE STATIC AND DYNAMIC ROTARY STABILITY DERIVATIVES AT SUBSONIC SPEEDS ON AN AIRPLANE MODEL HAVING WING AND TAIL SURFACES SWEPT BACK 45
260			_a _bNasa, Washington, D.C. _c1959
300			_a75
500			_aBound With Nasa Memo 5-12-59a,5-18-59a-5-20-59a Lack No. 13-15,17,19
700			_aTinling,Bruce E
964			_gCIRC
997			_aTR11440 C
999			_c396751 _d396751