Effect of apex strake incidence-angle on the vortex development and interaction of a double-delta wing
Author:
Publisher
Springer Science and Business Media LLC
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics
Link
http://link.springer.com/content/pdf/10.1007/s00348-009-0644-3.pdf
Reference18 articles.
1. AIAA Standard (1999) Assessment of experimental uncertainty with application to wind Tunnel testing. AIAA S-071A-1999
2. Barberis D, Molton P, Renac F, Mitchell AM (2004) Vortex control on delta wings. AIAA Paper 2004-2620, July 2004
3. Buter TA, Rao DM (1983) Experimental and computational investigation of an apex flap concept on a delta wing. NASA CR-166080
4. Grantz AC, Marchman JFIII (1983) Trailing edge flap influence on leading edge vortex flap aerodynamics. J Aircr 20(2):165–169
5. Gursul I, Srinivas S, Batta G (1995) Active control of vortex breakdown over a delta wing. AIAA J 33(9):1743–1745
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