Comparison of Euler and full potential marching techniques for flowsover complex configurations-Reference-Cited by-同舟云学术

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Comparison of Euler and full potential marching techniques for flowsover complex configurations

Published:1986-01-06 Issue: Volume: Page:
ISSN:
Container-title:24th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

SZEMA K.¹,CHAKRAVARTHY S.¹,SHANKAR V.¹,BYERLY J.¹

Affiliation:

1. Rockwell International Science Center, Thousand Oaks, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-244

Reference13 articles.

1. Conservative Type-Dependent Full Potential Method for the Treatment of Supersonic Flow with Imbedded Subsonic Region," AIAA Paper No. 83-1887, July 1983. 2. Szema, K.Y. and Shankar ,V. "Nonlinear

2. Computation of Wing-Body-Vertical Tail-Wake Flows at Low Supersonic Speed," AIAA Paper No. 84-0427, Jan. 1984. 3. Szema, K.Y., Riba, W.L., Shankar, V. and

3. Computation of supersonic flows over three-dimensional configurations

4. Euler solver for three-dimensional supersonic flows with subsonic pockets

5. Implicit treatment of the unsteady full potential equation in conservation form

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