000			00426pam a2200145a 44500
082			_aNASA _bTN D-2560
100			_aDavenport,E E
245	1		_aWIND-TUNNEL-WALL EFFECTS AND SCALE EFFECTS ON A VTOL CONFIGURATION WITH A FAN MOUNTED IN THE FUSELAGE.
260			_a _bNasa, Washington, D.C. _c1965
300			_a97
500			_aBound With Nasa Tn D-2551-2559
700			_aKuhn,R E
964			_gCIRC
997			_aTR10872 C
999			_c396011 _d396011