A fully implicit time accurate method for hypersonic combustion: application to shock-induced combustion instability

Author:

Yungster Shaye,Radhakrishnan Krishnan

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Reference24 articles.

1. Abgrall R (1989) Extension of Roe's Approximate Riemann Solver to Equilibrium and Nonequilibrium Flows. Proc. of the 8th GAMM-Conference on Numerical Methods in Fluid Mechanics, Delft, Netherlands, pp 1–10

2. Ahuja JK, Tiwari SN (1994) A Parametric Study of Shock-Induced Combustion in a Hydrogen-Air System. AIAA Paper 94-0674

3. Alpert RL, Toong, TY (1972) Periodicity in Exothermic Hypersonic Flows About Blunt Projectiles. Astr Acta 4–5:589–596

4. Behrens H, Struth W, Wecken F (1967) Shock-Induced Combustion by High-Speed Shots in Explosive Gas Mixtures. Institute Saint Louis (ISL) Rep 4/67, Saint Louis, France

5. Bruckner AP, Knowlen C, Hertzberg A, Bogdanoff DW (1991) Operational Characteristics of the Thermally Chocked Ram Accelerator. J Prop and Power 7:828–836

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