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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows

Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows - Elements in Aerospace Engineering

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Publisher's Synopsis

In this Element, the gas-particle flow problem is formulated with momentum and thermal slip that introduces two relaxation times. Starting from acoustical propagation in a medium in equilibrium, the relaxation-wave equation in airfoil coordinates is derived though a Galilean transformation for uniform flow. Steady planar small perturbation supersonic flow is studied in detail according to Whitham's higher-order waves. The signals owing to wall boundary conditions are damped along the frozen-Mach wave, and are both damped and diffusive along an effective-intermediate Mach wave and diffusive along the equilibrium Mach wave where the bulk of the disturbance propagates. The surface pressure coefficient is obtained exactly for small-disturbance theory, but it is considerably simplified for the small particle-to-gas mass loading approximation, equivalent to a simple-wave approximation. Other relaxation-wave problems are discussed. Martian dust-storm properties in terms of gas-particle flow parameters are estimated.

About the Publisher

Cambridge University Press

Cambridge University Press dates from 1534 and is part of the University of Cambridge. We further the University's mission by disseminating knowledge in the pursuit of education, learning and research at the highest international levels of excellence.

Book information

ISBN: 9781108964883
Publisher: Cambridge University Press
Imprint: Cambridge University Press
Pub date:
DEWEY: 533.2
DEWEY edition: 23
Language: English
Number of pages: 66
Weight: 126g
Height: 152mm
Width: 229mm
Spine width: 10mm