On modem military air vehicles, high lift systems are used to improve takeoff and landing performance. For naval air vehicles, an improvement in the lift coefficient of a landing or approach configuration allows for arrested landings at reduced speeds or the ability to carry more weight back to the ship. For conventional takeoff or landing (CTOL), improved lift to drag ratios allow for shorter takeoff runs or greater payload capacity.
Low-Speed Wind Tunnel Tests on a Diamond Wing High Lift Configuration
2000
5 pages
Report
No indication
English
AIAA-2004-4843 Low-Speed Wind Tunnel Tests on a Lambda Wing High-Lift Configuration
British Library Conference Proceedings | 2004
|Low-speed wind tunnel tests of a high-lift supersonic wing
TIBKAT | 1950
|Wind-tunnel tests of hall high-lift wing
Engineering Index Backfile | 1932
|