Flows over blunt bodies using a flux-splitting and shock-fitting scheme-Reference-Cited by-同舟云学术

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Flows over blunt bodies using a flux-splitting and shock-fitting scheme

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

Author:

SCHERR S.¹,SHANG J.¹

Affiliation:

1. USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-340

Reference19 articles.

1. Finite-volume solutions to the Euler equations in transonic flow

2. Workshop on the Development and Applications of the AFWAL Psrabolized Navier-Stokes Code, May 11-13, 1983, Dayton, OH.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical study of hypersonic dissociated air past blunt bodies;AIAA Journal;1991-05

2. Unsteady heat transfer coefficient estimation for long duration;Journal of Thermophysics and Heat Transfer;1988-07

3. Numerical simulations of non-equilibrium hypersonic flow past blunt bodies;26th Aerospace Sciences Meeting;1988-01-11

4. Hypersonic flow past 3-D configurations;25th AIAA Aerospace Sciences Meeting;1987-03-24

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