·· .. ;.. RE P 0 R T 0 F

First Page		Document Content
Date: 2013-03-11 16:30:40 Aerodynamics National Advisory Committee for Aeronautics Fred Weick Langley Research Center Wind tunnel Stall Spin Robert T. Jones Deflected slipstream Aviation Transport Flight		·· .. ;.. RE P 0 R T 0 F Add to Reading List Source URL: crgis.ndc.nasa.gov Download Document from Source Website File Size: 3,65 MB Share Document on Facebook

	AIAA1st Flow Control ConferenceJune 2002, St. Louis, Missouri AIAA DocID: 1aX7Z - View Document
	Wichita State University Libraries Department of Special Collections UNIVERSITY ARCHIVES[removed]University of Wichita Engineering Reports (UWER) Box 1 DocID: LI1Q - View Document
	Flight validation of cruise efficient, low noise, Extreme short takeoff and landing (CESTOL) and circulation control (CC) for drag reduction enabling technologies Investigators: Bruce Cogan NASA DFRC (PI), Nhan Nguyen NA DocID: FGcx - View Document
	FREE-FLIGHT TUNNEL Project No. 2 Brewster XF2A-1 Tested by Joseph A. Shortal HISTORY The Brewster XF2A-1 airplane was a midwing type navy shipboard fighter airplane with a DocID: E8w8 - View Document
	·· .. ;.. RE P 0 R T 0 F DocID: xxYg - View Document