000			00559pam a2200133a 44500
082			_aNASA _bNEMO 1-27-59L
100			_aGainer,Thomas G
245	1		_aLOW-SPEED WIND-TUNNEL INVESTIGATION TO DETERMINE THE AERODYNAMIC CHARACTERISTICS OF A RECTANGULAR WING EQUIPPED WITH A FULL-SPAN AND AN INBOARD HALF-SPAN JET-AUGMENTED FLAP DEFLECTED 55 DEGREE
260			_a _bNasa, Washington, D.C. _c1959
300			_a21
500			_aBound With Nasa Memo 1-15-59l-26,30-31, Lack No.1-18-59l-1-19-59l,1-21-59l,1-28-59l-1-29-59l
964			_gCIRC
997			_aTR17741 C
999			_c400899 _d400899