000			00509pam a2200121a 44500
082			_aNASA _bMEMO 5-20-59L
100			_aHewes,Donald E
245	1		_aLOW-SUBSONIC MEASUREMENTS OF THE STATIC AND OSCILATORY LATERAL STABILITY DERIVATIVES OF A SWEPTBACK-WING AIRPLANE CONFIGURATION AT ANGLES OF ATTACK FROM-10 D/C TO 90 D/C
260			_a _bNasa, Washington, D.C. _c1959
500			_aBound With Nasa Memo 5-12-59l-5-18-59l And 5-23-59l-28 Lack No.14-17, 19, 21-22, And 27
964			_gCIRC
997			_aTR7407 C
999			_c395826 _d395826