Numerical Investigation of a Blunt-Nosed Elliptical Cone at High Angle of Attack in Nonequilibrium Flow-Reference-Cited by-同舟云学术

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Numerical Investigation of a Blunt-Nosed Elliptical Cone at High Angle of Attack in Nonequilibrium Flow

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA Fluid Dynamics Conference
language:
Short-container-title:

Author:

Atkinson Michael¹,Poggie Jon¹,Camberos Jose¹

Affiliation:

1. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4052

Reference22 articles.

1. High Angle-of-Attack Aerodynamics

2. Hankey, Wilbur, L., Re-entryAerodynamics, AIAAEducationalSeries, Washington, DC,1988.

3. Stetson,K.F."Experimental ResultsofLaminar BoundaryLayer SeparationonaSlender ConeatAngleofAttackat M∞=14.2,"AerospaceResearchLaboratories,ARL71-0127,Aug.1971.

4. Nowlan, D. T.,Pressureand Heat Transfer Distributionon ASDEllipticCone(W3) and ASDSortie(W4) in theCAL 48-Inch HypersonicShockTunnel, AM-1800-Y-2,1964.

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1. Numerical Investigation of a Blunt-Nosed Elliptical Cone at High Angle of Attack in Nonequilibrium Flow;39th AIAA Fluid Dynamics Conference;2009-06-14

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