A Computational Study on the Effect of Chine Nose Shapes on a Slender Body Flight Vehicle at High Angles of Attack-Reference-Cited by-同舟云学术

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A Computational Study on the Effect of Chine Nose Shapes on a Slender Body Flight Vehicle at High Angles of Attack

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Lim Seol¹,Kim Sang Dug²,Song Dong Joo³

Affiliation:

1. Yeungnam University

2. UNISON Co., Ltd.

3. Yeongnam University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1044

Reference9 articles.

1. 2B.L.Hunt,"AsymmetricVortexForcesandWakesonSlenderBodies,"AIAA,Atmospheric Flight MechanicsConference,9th,SanDiego,CA,Aug9-11,1982,42 pp.

2. Maximum vortex-induced side force revisited

3. 5Ericsson,L.E.andReding,J.P."Vortex-InducedAsymmetricLoadsin2-Dand3-DFlows," AIAA,AerospaceSciencesMeeting,18th, Pasadena,Calif.,Jan14-16,1980,46pp.

Cited by 1 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. Effect of multiple rings on side force over an ogive-cylinder body at subsonic speed;Chinese Journal of Aeronautics;2018-06

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