Accuracy of Parabolized Navier-Stokes Schemes for Stability Analysis of Hypersonic Axisymmetric Flows-Reference-Cited by-同舟云学术

Accuracy of Parabolized Navier-Stokes Schemes for Stability Analysis of Hypersonic Axisymmetric Flows

Published:2002-07 Issue:7 Volume:40 Page:1311-1322
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Esfahanian Vahid¹,Hejranfar Kazem¹

Affiliation:

1. University of Tehran, 11365-4563 Tehran, Iran

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1820

Reference28 articles.

1. 1Stetson, K. F. “Effect of Bluntness and Angle of Attack on Boundary-Layer Transition on Cone and Biconic Configuration,”AIAA Paper 79-0269, Jan. 1979.

2. Effect of nose bluntness on boundary layer stability and transition

3. 4Esfahanian, V. “Computation and Stability Analysis of Laminar Flow over a Blunted Cone in Hypersonic Flow,” Ph.D. Dissertation, Dept. of Aeronautical and Astronautical Engineering,The Ohio State Univ., Columbus, OH,June 1991.

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