000			00536pam a2200145a 44500
082			_aNASA _bCR-373 -
100			_aHiggins,C C, Kelly,D P
245	1		_aEXHAUST JET WAKE AND THRUST CHARACTERISTICS OF SEVERAL NOZZLES DESIGNED FOR VTOL DOWNWASH SUPPRESSION _cTESTS IN AND OUT OF GROUND EFFECT WITH 70(DEGREE) F AND 1200(DEGREE) F NOZZLE DISCHARGE TEMPERATURES
260			_a _bNasa, Washington, D.C. _c1966
300			_a97
500			_aBound With Nasa Cr-371-376
700			_aWainwright,T W
964			_gCIRC
997			_aTR8930 C
999			_c393829 _d393829