000			00531pam a2200145a 44500
082			_aNASA _bMEMO 4-22-59L
100			_aSpencer,Bernard
245	1		_aLOW-SPEED LONGITUDINAL CHARACTERISTICS OF AN AIRPLANE CONFIGURATION INCLUDING EFFECTS OF CANARD AND WING TRAILING-EDGE FLAP CONTROLS IN COMBINATION
260			_a _bNasa, Washington, D.C. _c1959
300			_a50
500			_aBound With Nasa Memo 4-20-59l-4-21-59l And 4-23-59l-4-30-59l Lack No.24and29
700			_aSleeman,William C
964			_gCIRC
997			_aTR7401 C
999			_c395617 _d395617