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The fundamentals of linear and nonlinear waves in gas-particle flows are studied, emphasizing the relaxation processes in such a mixture.
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows
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Cambridge University Press, 2021
ISBN 10: 1108964885
ISBN 13: 9781108964883
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows
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Cambridge University Press, 2021
ISBN 10: 1108964885
ISBN 13: 9781108964883
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows (Elements in Aerospace Engineering)
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows
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Condizione: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Gas-particle flows became relevant in Aerospace Engineering owing to small solid particle additives to alleviate acoustical instabilities in solid propellant rocket motors, thereby motivating the study of a variety of nonlinear and linear waves. Emphasis is. Codice articolo 438754458
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows (Elements in Aerospace Engineering)
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows (Elements in Aerospace Engineering)
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows (Elements in Aerospace Engineering)
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows
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Cambridge University Press 2021-09, 2021
ISBN 10: 1108964885
ISBN 13: 9781108964883
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows (Paperback)
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Cambridge University Press, Cambridge, 2021
ISBN 10: 1108964885
ISBN 13: 9781108964883
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Paperback. Condizione: new. Paperback. 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. Gas-particle flows became relevant in Aerospace Engineering owing to small solid particle additives to alleviate acoustical instabilities in solid propellant rocket motors, thereby motivating the study of a variety of nonlinear and linear waves. Emphasis is placed on fundamental aspects of the relaxation nature of the flow processes. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. Codice articolo 9781108964883
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Mach Wave and Acoustical Wave Structure in Nonequilibrium Gas-Particle Flows (Paperback)
Editore:
Cambridge University Press, Cambridge, 2021
ISBN 10: 1108964885
ISBN 13: 9781108964883
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Paperback
Da: AussieBookSeller, Truganina, VIC, Australia
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Paperback. Condizione: new. Paperback. 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. Gas-particle flows became relevant in Aerospace Engineering owing to small solid particle additives to alleviate acoustical instabilities in solid propellant rocket motors, thereby motivating the study of a variety of nonlinear and linear waves. Emphasis is placed on fundamental aspects of the relaxation nature of the flow processes. Shipping may be from our Sydney, NSW warehouse or from our UK or US warehouse, depending on stock availability. Codice articolo 9781108964883
Quantità: 1 disponibili