Effect of duct geometry on shock wave discharge

Author:

Kweon Y. -H.,Miyazato Y.,Aoki T.,Kim H. -D.,Setoguchi T.

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference18 articles.

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2. Sekine, N.; Matsumura, S.; Aoki, K.; Takayama, K.: Generation and propagation of shock waves in the exhaust pipe of a four cycle automobile engine, 17th International Sympo-sium on Shock Wave and Shock Tubes, Bethlehem, pp. 671–676, (1989)

3. Matsuo, K.; Aoki, T.: Wave problems in high-speed rail-way tunnel, 18th International Symposium on Shock Wave and Shock Tubes, Sendai, 1992)

4. Adamson, T. C. Jr.; Nicholls, A.: On the structure of jets from highly underexpanded nozzles into still air, J. Aerospace Sciences, vol. 26, pp. 16–24, (1959)

5. Sherman, F. S.: The structure and utilization of supersonic free jets in low density wind tunnels, Rarefied Gas Dynamics, Academic Press, New York, Vol. 2, pp. 84–105, (1966)

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1. On the Unsteady Shock Wave Interaction with a Backward-Facing Step: Inviscid Analysis;42nd AIAA Fluid Dynamics Conference and Exhibit;2012-06-25

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