SIDE-FORCE CONTROL ON A DIAMOND FOREBODY AT HIGH ANGLES OF ATTACK

Authors
Citation
Dm. Rao et G. Sharma, SIDE-FORCE CONTROL ON A DIAMOND FOREBODY AT HIGH ANGLES OF ATTACK, Journal of aircraft, 31(4), 1994, pp. 915-921
Citations number
NO
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00218669
Volume
31
Issue
4
Year of publication
1994
Pages
915 - 921
Database
ISI
SICI code
0021-8669(1994)31:4<915:SCOADF>2.0.ZU;2-6
Abstract
A high-alpha side-force control concept for diamond cross section fore bodies was investigated. A full-length strake is deployed on one of th e lower facets to force a large-scale separation vortex adjacent to th e forebody surface, whose suction provides side force across a broad h igh-alpha range. A simultaneous reduction of the leeside vortex suctio n decreases the forebody normal force, leading to pitch-up alleviation and drag reduction as additional high-alpha benefits, particularly wh en the strakes are deployed on both sides. Low-speed wind-tunnel measu rements of surface pressures and six-component forces/moments supporte d by surface and flowfield visualizations on an isolated diamond foreb ody model verified the control effectiveness to nearly 70-deg angle of attack, and up to 10-deg sideslip angle.