First Page | Document Content | |
---|---|---|
![]() Date: 2013-03-11 16:30:40Aerodynamics National Advisory Committee for Aeronautics Fred Weick Langley Research Center Wind tunnel Stall Spin Robert T. Jones Deflected slipstream Aviation Transport Flight | Add to Reading List |
![]() | AIAA1st Flow Control ConferenceJune 2002, St. Louis, Missouri AIAADocID: 1aX7Z - View Document |
![]() | Wichita State University Libraries Department of Special Collections UNIVERSITY ARCHIVES[removed]University of Wichita Engineering Reports (UWER) Box 1DocID: 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 NADocID: 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 aDocID: E8w8 - View Document |
![]() | ·· .. ;.. RE P 0 R T 0 FDocID: xxYg - View Document |