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Aerodynamics / Aerospace engineering / Mach reflection / Shock wave / Mach number / Speed of sound / Mach wave / Fluid dynamics / Dynamics / Fluid mechanics


J. Fluid Mech[removed]), vol. 750, pp. 385_400. c Cambridge University Press 2014 doi:[removed]jfm[removed]Dynamic transition from Mach to regular reflection of shock waves in a steady flow K. Naidoo1 and B. W. Skews2,†
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Document Date: 2014-12-03 16:55:15


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City

Pretoria / /

Company

Cambridge University Press / /

Country

South Africa / /

Facility

Africa University / /

Organization

Cambridge University / Council for Scientific and Industrial Research / South 2Flow Research Unit / Africa University of the Witwatersrand / Johannesburg / School of Mechanical / Industrial and Aeronautical Engineering / /

Technology

constant angular velocity / /

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