Experimental and numerical study of shock wave attenuation at the outlet of two-dimensional and axisymmetric ducts-Reference-Cited by-同舟云学术

Experimental and numerical study of shock wave attenuation at the outlet of two-dimensional and axisymmetric ducts

Published:1993-07 Issue:4 Volume:28 Page:590-593
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Bazhenova T. V.,Bazarov S. B.,Bulat O. V.,Golub V. V.,Schul'meister A. M.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/article/10.1007/BF01342697/fulltext.html

Reference5 articles.

1. T. V. Bazhenova and L. G. Gvozdeva,Unsteady Interactions of Shock Waves [in Russian], Nauka, Moscow (1977).

2. K. C. Phan and J. L. Stollery, ?The effect of suppressors and muzzle brakes on shock wave strength,? in:Proc. 14th Int. Symp. on Shock Tubes and Shock Waves, Sydney, 1983, Liverpool (1983), p. 519.

3. A. Abe and K. Takayama, ?Shock wave discharged from the open end of a shock tube,? in:Proc. Nat. Symp. on Shock Wave Phenomena, Japan, 1988, Sendai (1989), p. 41.

4. R. Hillier, ?Computation of shock wave diffraction at a ninety degree convex edge,?Shock Waves,1, 89 (1991).

5. T. V. Bazhenova, L. G. Gvozdeva, and Yu. V. Zhilin, ?Change in shock wave strength on diffraction at a convex corner,?Teplofiz. Vys. Temp.,14, 436 (1976).

Cited by 5 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 and experimental study of shock waves emanating from an open-ended rectangular tube;Shock Waves;2016-04-28

2. Half a century of continuous shock interaction investigations in the Joint Institute for High Temperatures of Russian Academy of Sciences;Shock Waves;2014-02-19

3. On the Unsteady Shock Wave Interaction with a Splitter Plate: Inviscid Analysis;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05

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

5. Theory of unsteady separation in supersonic flow around a convex corner;Fluid Dynamics;2007-06