000			01000pam a2200217a 44500
003			OSt
040			_cIIT Kanpur
041			_aeng
110			_aWashington. National Aeronautics and Space Administration (NASA)
245	1		_aNASA Memorandum [NASA MEMO 4-21-59A]: Longitudinal stability and control characteristics at mach numbers from 0.70 to 2.22 of a triangular wing configuration equipped with a canard control, a trailing-edge-flap control or a cambered forebody _cJohn W. Boyd and Gene P. Menees
260			_bNASA _c1959 _aWashington
300			_a39p
440			_aNational Aeronautics and Space Administration
440			_aNASA Memorandum
500			_aBound together NASA MEMO 4-14-59A to 4-27-59A Lack No.4-16 to 4-17, 4-22 to 4-25
500			_aBound vol. Acc. No. 102439 contains Acc. No. TR11609 to TR11615
650			_aLongitudinal control devices --Tests
700			_aBoyd, John W.
700			_aMenees, Gene P.
942			_cBK
999			_c397618 _d397618