Introduction to Compressible Fluid Flow (2nd Ed.) Heat Transfer Series
Auteurs : Oosthuizen Patrick H., Carscallen William E.
Introduction to Compressible Fluid Flow, Second Edition offers extensive coverage of the physical phenomena experienced in compressible flow. Updated and revised, the second edition provides a thorough explanation of the assumptions used in the analysis of compressible flows. It develops in students an understanding of what causes compressible flows to differ from incompressible flows and how they can be analyzed. This book also offers a strong foundation for more advanced and focused study.
The book begins with discussions of the analysis of isentropic flows, of normal and oblique shock waves and of expansion waves. The final chapters deal with nozzle characteristics, friction effects, heat exchange effects, a hypersonic flow, high-temperature gas effects, and low-density flows. This book applies real-world applications and gives greater attention to the supporting software and its practical application.
- Includes numerical results obtained using a modern commercial CFD (computer fluid dynamics) code to illustrate the type of results that can be obtained using such a code
- Replaces BASIC language programs with MATLAB® routines
- Avails COMPROP2 software which readers can use to do compressible flow computation
Additional problems have been added, and non-numerical problems illustrating practical applications have been included. A solutions manual that contains complete solutions to all of the problems in this book is available. The manual incorporates the same problem-solving methodology as adopted in the worked examples in this book. It also provides summaries of the major equations developed in each chapter. An interactive computer program also accompanies this book.
Introduction. The Equations of Steady One-Dimensional Compressible Flow. Some Fundamental Aspects of Compressible Flow. One-Dimensional Isentropic Flow. Normal Shock Waves. Oblique Shock Waves. Expansion Waves - Prandtl-Meyer Flow. Variable Area Flows. Adiabatic Flow with Friction. Flow with Heat Transfer. Linearized Analysis of Two-Dimensional Compressible Flows. Hypersonic and High-Temperature Flows. High-Temperature Gas Effects. Low-Density Flows. Bibliography. Appendices.
Patrick H. Oosthuizen is a professor of mechanical engineering at Queen’s University in Kingston, Ontario, Canada. He received BSc(Eng), MSc(Eng), and PhD degrees in mechanical engineering from the University of Cape Town, South Africa, and an MASc degree in aerospace engineering from the University of Toronto, Canada. He joined Queen’s University after teaching for several years at the University of Cape Town. His research is in the areas of heat transfer, fluid mechanics, and energy systems. He has authored more than 600 technical publications in journals and conference proceedings, and has received a number of teaching and research awards.
William E. Carscallen
Date de parution : 09-2013
Ouvrage de 416 p.
17.8x25.4 cm
Thèmes d’Introduction to Compressible Fluid Flow :
Mots-clés :
Mach Number; Pitot Static Tube; HYPERSONIC FLOW; Normal Shock Wave; VARIABLE AREA VIEW; Normal Shock; EXPANSION WAVES; Oblique Shock Wave; SHOCK WAVES; Normal Shock Relations; COMPRESSIBILITY; Combustion Chamber; Convergent Divergent Nozzle; Constant Area Duct; Stagnation Pressure; Oblique Shock; Nozzle Exit Plane; Isentropic Flow; Compressible Fluid Flows; Exit Mach Number; Supersonic Flow; Stagnation Temperature; Isentropic Relations; Mass Flow Rate; Mach Wave; Supersonic Wind Tunnel; Shock Wave; Control Volume; Inlet Mach Number; Compressible Gas Flows