000			00498pam a2200133a 44500
082			_aNASA _bTN D-1245
100			_aSpencer,Bernard
245	1		_aLOW-SPEED AERODYNAMIC CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION HAVING SPLIT FLAPS LOCATED AHEAD OF THE WING TRAILING EDGE AND LEADING-AND TRAILING -EDGE FLAPS ON THE CANARD CONTROL
260			_a _bNasa, Washington, D.C. _c1962
300			_a54
500			_aBound With Nasa Tn D-1241-44, 1246-50
964			_gCIRC
997			_aTR12804 C
999			_c397820 _d397820