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Numerical Simulation of Viscous Shock Layer Flows - Fluid Mechanics and Its Applications Y.P. Golovachov Softcover reprint of hardcover 1st ed. 1995 edition
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Numerical Simulation of Viscous Shock Layer Flows - Fluid Mechanics and Its Applications
Y.P. Golovachov
The flow field around a body moving at supersonic speed can be divided into three parts, namely, shock layer, near wake including base flow, and far wake. The shock layer flow is bounded by the bow shock wave and the front and lat eral parts of the body surface.
346 pages, biography
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