A Computational Study on The Effect of Asymmetric Laminar-Turbulent Transition Conditions on a Tangent-Ogive-Cylinder Flight Vehicle at the High Angles of Attack-Reference-Cited by-同舟云学术

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A Computational Study on The Effect of Asymmetric Laminar-Turbulent Transition Conditions on a Tangent-Ogive-Cylinder Flight Vehicle at the High Angles of Attack

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:38th Fluid Dynamics Conference and Exhibit
language:
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Author:

Lim Seol¹,Kim Sang Dug²,Song Dong Joo¹

Affiliation:

1. Yeungnam University

2. Daegu University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-4071

Reference9 articles.

1. 3B.L.Hunt,"AsymmetricVortexForcesandWakesonSlenderBodies,"AIAA,Atmospheric Flight MechanicsConference,9th,San Diego,CA,Aug9-11,1982,42 pp.

2. 5Ericsson,L.E.andReding,J.P."Vortex-InducedAsymmetricLoadsin2-Dand3-DFlows," AIAA,Aerospace SciencesMeeting,18th, Pasadena,Calif.,Jan14-16,1980,46pp.

3. Maximum vortex-induced side force revisited

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1. A Computational Study on the Effect of Chine Nose Shapes on a Slender Body Flight Vehicle at High Angles of Attack;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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