000			00974pam a2200217a 44500
003			OSt
040			_cIIT Kanpur
041			_aeng
110			_aWashington. National Aeronautics and Space Administration (NASA)
245	1		_aNASA Memorandum [NASA MEMO 4-20-59A]: Static stability and control of canard configurations at mach numbers from 0.70 to 2.22- lateral-directional characteristics of an unswept wing and canard _cVictor L. Peterson
260			_bNasa, Washington, D.C. _c1959
300			_a32p
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			_aCanard airplane configurations
650			_aCanard airplane --Sstatic stability and control
700			_aPeterson, Victor L.
942			_cBK
999			_c397617 _d397617