000			00539pam a2200145a 44500
082			_aNASA _bMEMO 5-20-59A
100			_aMenees,Gene P
245	1		_aAN EXPERIMENTAL INVESTIGATION OF THE EFFECT OF A CANARD CONTROL ON THE LIFT, DRAG, AND PITCHING MOMENT OF AN ASPECT-RATIO-2.O TRIANGULAR WING INCORPORATING A FORM OF CONICAL CAMBER
260			_a _bNasa, Washington, D.C. _c1959
300			_a29
500			_aBound With Nasa Memo 5-12-59a-5-18-59a Lack No.13-15,17,19
700			_aBoyd,John W
964			_gCIRC
997			_aTR11442 C
999			_c396753 _d396753