000			00458pam a2200145a 44500
082			_aNASA _bTN D-1509
100			_aWinston,M M
245	1		_aPROPELLER SLIPSTREAM EFFECTS AS DETERMINED FROM WING PRESSURE DISTRIBUTION ON A LARGE-SCALE SIX-PROPELLER VTOL MODEL AT STATIC THRUST
260			_a _bNasa, Washington, D.C. _c1962
300			_a67
500			_aBound With Nasa Tn D-1501-1508.
700			_aHuston,R J
964			_gCIRC
997			_aTR11473 C
999			_c397601 _d397601