000			00506pam a2200145a 44500
082			_aNASA _bMEMO 4-4-59L -
100			_aSpearman,M Leroy
245	1		_aEFFECTS OF FOREBODY DEFLECTION ON STABILITY AND CONTROL CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION WITH A HIGH TRAPEZOIDAL WING AT A MACH NUMBER OF 2.01
260			_a _bNasa, Washington, D.C. _c1959
300			_a28
500			_aBound With Nasa Memo 4-1-59l-4-19-59l
700			_aDriver,Cornelius
964			_gCIRC
997			_aTR7689 C
999			_c393202 _d393202