Numerical Simulation of Viscous Shock Layer Flows (Fluid Mechanics and Its Applications)

New
Hardcover
1995
$284.73

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.

Synopsis

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.

$284.73

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20+ in stock

More Information

Format: Hardcover
Pages: 364
Publisher: Springer
Published: 30 Sep 1995
ISBN 10: 0792336267
ISBN 13: 9780792336266

Numerical Simulation of Viscous Shock Layer Flows (Fluid Mechanics and Its Applications)

New

$284.73

Synopsis

$284.73

More Information