Author:
Zhang Guang,Setoguchi Toshiaki,Kim Heuy Dong
Publisher
Springer Science and Business Media LLC
Reference15 articles.
1. Duff. R. E., “Shock Tube Performance at Initial Low Pressure,” Phys. Fluids, vol. 2, 1959, pp. 207–216.
2. Brouillete. M., “Shock Waves at Microscales,” Shock Waves, vol. 13, 2003, pp. 3–12.
3. Mirels. H., “Test Time in Low Pressure Shock Tube,” Phys. Fluids, vol. 6, 1963, pp. 1201–1214.
4. Sturtevant. B. and Okamura. T. T., “Dependence of Shock Tube Boundary Layers on Shock Strength,” Phys. Fluids, vol. 12, 1969, pp. 1723–1725.
5. Kohsuke Tanaki, Kazuaki Inaba and Makoto Yamamoto, “Numerical Investigation on Transition of Shock Induced Boundary Layer,” 47th AIAA Aerospace Science Meeting Including the New Horizons Forum and Aerospace Exposition, January 2009, Orlando, Florida.
Cited by
11 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