Hodograph solution for compressible flow past a corner and comparison with Euler numerical predictions-Reference-Cited by-同舟云学术

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Hodograph solution for compressible flow past a corner and comparison with Euler numerical predictions

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:10th Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

VERHOFF A.¹,STOOKESBERRY D.¹,MICHAL T.¹

Affiliation:

1. McDonnell Aircraft Co., Saint Louis, MO

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1547

Reference9 articles.

1. Van Dyke, M. =Second-Order SubsonicAirfoil Theory Including EdgeEffects," NACAReport No. 1274, 1956.

2. Salas, M. D. *Foundations for the Numerical Solution of the Euler Equations," in Advances k putational Transonics, Pineridge Press, 1985, pp.343-369.

3. Jameson, A, KAVertex Based Multigrid Algorithm for Three-Dimensional Flow Calculations,' ASME AMDVol.78, Dec. 1986, pp.45-73.

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2. Flow Similarity in Compressible Convex-Corner Flows;AIAA Journal;2012-04

3. Inviscid-Viscous Interactions of Compressible Convex Corner Flows;28th International Symposium on Shock Waves;2012

4. Effect of Normal Blowing on Compressible Convex-Corner Flows;Journal of Aircraft;2010-07

5. Analytical Euler Solution for Two Dimensional Compressible Ramp Flow with Experimental Comparison;AIAA Journal;2004-05

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