Articoli correlati a Gas Dynamics: Key Equations and Tables
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This book is a valuable supplementary resource for courses on gas dynamics and compressible flows. It provides concise summaries of key equations for various flow functions, isentropic flow, Fanno flow, Rayleigh flow, isothermal constant-area flow with friction, normal and oblique shocks, and Prandtl-Meyer flow. Additionally, it includes tables that relate these flows to Mach numbers, from subsonic to hypersonic, for specific heat ratios of 1.4 and 1.333. Instructors can utilize this book during closed-book exams, enabling students to access essential equations and tables for solving problems.
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Gas Dynamics: Key Equations and Tables
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Gas Dynamics
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Gas Dynamics (Paperback)
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Paperback. Condizione: new. Paperback. This book is a valuable supplementary resource for courses on gas dynamics and compressible flows. It provides concise summaries of key equations for various flow functions, isentropic flow, Fanno flow, Rayleigh flow, isothermal constant-area flow with friction, normal and oblique shocks, and Prandtl-Meyer flow. Additionally, it includes tables that relate these flows to Mach numbers, from subsonic to hypersonic, for specific heat ratios of 1.4 and 1.333. Instructors can utilize this book during closed-book exams, enabling students to access essential equations and tables for solving problems. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. Codice articolo 9798242276161
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Gas Dynamics
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PAP. Condizione: New. New Book. Shipped from UK. Established seller since 2000. Codice articolo L2-9798242276161
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Gas Dynamics (Paperback)
Print on DemandDa: CitiRetail, Stevenage, Regno Unito
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Paperback. Condizione: new. Paperback. This book is a valuable supplementary resource for courses on gas dynamics and compressible flows. It provides concise summaries of key equations for various flow functions, isentropic flow, Fanno flow, Rayleigh flow, isothermal constant-area flow with friction, normal and oblique shocks, and Prandtl-Meyer flow. Additionally, it includes tables that relate these flows to Mach numbers, from subsonic to hypersonic, for specific heat ratios of 1.4 and 1.333. Instructors can utilize this book during closed-book exams, enabling students to access essential equations and tables for solving problems. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. Codice articolo 9798242276161
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