The Proceedings of the Fluids engineering conference
Online ISSN : 2424-2896
2007
Session ID : 406
Conference information
406 Effect of Pressure Ratio and Exit Mach Number for Hysteresis Phenomenon of Shock Wave in Axisymmetric Over-Expanded Supersonic Jet(1)
Tsuyoshi Yasunobu, Yumiko Otobe, Hideo Kashimura, Toshiaki Setoguchi
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Keywords: Compressible Flow, Axisymmetric Flow, Overexpanded Supersonic Jet, Regular Reflection, Mach Reflection
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© 2007 The Japan Society of Mechanical Engineers
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