Computational Fluid Dynamics Algorithms for Unsteady Shock-Induced Combustion, Part 1: Validation-Reference-Cited by-同舟云学术

Computational Fluid Dynamics Algorithms for Unsteady Shock-Induced Combustion, Part 1: Validation

Published:2000-07 Issue:7 Volume:38 Page:1179-1187
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Choi Jeong-Yeol¹,Jeung In-Seuck²,Yoon Youngbin²

Affiliation:

1. Pusan National University, Pusan 609-735, Republic of Korea

2. Seoul National University, Seoul 151-742, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1112

Reference19 articles.

1. Detonation Waves and Propulsion

2. Ram accelerator - A new chemical method for accelerating projectilesto ultrahigh velocities

3. 4Toong,T. Y. “Chapter 10. Mechanisms of CombustionInstability,”Combustion Dynamics: The Dynamic of Chemically Reacting Fluids, McGraw-Hill, New York, 1983, pp.221-277.

4. Numerical simulation of shock-induced combustion around an axisymmetric blunt body

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