Experimental Investigations on Stability of Vortex Flow over Slender Delta Wing with Dorsal Fin-Reference-Cited by-同舟云学术

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Experimental Investigations on Stability of Vortex Flow over Slender Delta Wing with Dorsal Fin

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Meng Xuanshi¹,Cai Jinsheng¹,Qiao Zhide¹,Luo Shijun²,Liu Feng²

Affiliation:

1. Northwestern Polytechnical University

2. University of California, Irvine

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-486

Reference15 articles.

1. Sources of High Alpha Vortex Asymmetry at Zero Sideslip

2. Symmetry breaking in vortex flows on conical bodies

3. 3Shanks, R. "Low-subsonic Measurements of Static and Dynamic Stability Derivatives of Six Flat-plate Wing Having Leading-edgeSweep Angles of70 degto 84deg," NASA TN D-1822,July1963.

4. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy

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