Experimental Investigation of Vortex Flow of a Yawed Delta Wing Having Leading Edge Extension
Author:
Affiliation:
1. Korean Air Force Academy
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-3267
Reference8 articles.
1. Experimental and numerical investigation of vortex flow over a sideslipping delta wing
2. Double-delta-wing aerodynamics for pitching motions with and without sideslip
3. Vortex Characteristics of Pitching Double-Delta Wings
4. Control of High-Incidence Vortical Flow on Double-Delta Wings Undergoing Sideslip
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. PIV and CFD Analyses of Vortical Flow over a Yawed LEX-Delta Wing Configuration;23rd AIAA Applied Aerodynamics Conference;2005-06-06
2. Vortical flows over a LEX-delta wing at high angles of attack;KSME International Journal;2004-12
3. Vortical flows over a delta wing at high angles of attack;KSME International Journal;2004-06
4. Vortex Flow Visualization of a Yawed Delta Wing with Leading Edge Extension;Journal of Aircraft;2004-03
5. Velocity Measurements in Vortical Flow of a LEX-Delta Wing Configuration in a Sideslip;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05
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