Study on shock wave and turbulent boundary layer interactions in a square duct at Mach 2 and 4

Author:

Sugiyama Hiromu,Minato Ryojiro,Mizobata Kazuhide,Tojo Akira,Muto Yohei

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference11 articles.

1. Matsuo, K., Miyazato, Y., Kim, H.D. The Mechanism of Pseudo-Shocks Phenomena in Internal Gas Flows. Progress in Aerospace Sciences, 1999, 35: 33–100

2. Carroll, B F, Dutton, J C. Characteristics of Multiple Shock Wave/Turbulent Boundary-Layer Interactions in Rectangular Ducts. Journal of Propulsion and Power, 1990, 6(2): 186–193

3. Om, D, Childs, M E. Multiple Transonic Shock-Wave/Turbulent Boundary Layer Interaction in a Circular Duct. AIAA Journal, 1985, 23: 1506–1511

4. Sugiyama, H, Takeda, H, Zhang, J, et al. Multiple Shock Wave and Turbulent Boundary Layer Interaction in a Rectangular Duct. In: Proc. of 16th Int. Symp. on Shock Tubes and Waves, Aachen, 1987. 185–191

5. Sugiyama, H, Takeda, H, Zhang, J, et al. Locations and Oscillation Phenomena of Pseudo-Shock Waves in a Straight Rectangular Duct. JSME Int. J., Series II, 1988, 31(1): 9–15

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