Anderson's book provides the most accessible approach to compressible flow for Mechanical and Aerospace Engineering students and professionals. In keeping with previous versions, the 3rd edition uses numerous historical vignettes that show the evolution of the field. New pedagogical features--"Roadmaps" showing the development of a given topic, and "Design Boxes" giving examples of design decisions--will make the 3rd edition even more practical and user-friendly than before. The 3rd edition strikes a careful balance between classical methods of determining compressible flow, and modern numerical and computer techniques (such as CFD) now used widely in industry & research. A new Book Website will contain all problem solutions for instructors.

1 Compressible Flow - Some History and Introductory Thoughts

2 Integral Forms of the Conservation Equations for Inviscid Flows 

3 One-Dimensional Flow 

4 Oblique Shock and Expansion Waves 

5 Quasi-One-Dimensional Flow 

6 Differential Conservation Equations for Inviscid Flows 

7 Unsteady Wave Motion 

8 General Conservation Equations Revisited: Velocity Potential Equation 

9 Linearized Flow 

10 Conical Flow 

11 Numerical Techniques for Steady Supersonic Flow 

12 The Time-Marching Technique: With Application to Supersonic Blunt Bodies and Nozzles 

13 Three-Dimensional Flow 

14 Transonic Flow 

15 Hypersonic Flow 

16 Properties of High-Temperature Gases 

17 High-Temperature Flows: Basic Examples Appendix A Appendix B An Illustration and Exercise of Computational Fluid Dynamics

John D. Anderson, Jr. is the Curator of Aerodynamics at the National Air & Space Museum Smithsonian Institute and Professor Emeritus at the University of Maryland.

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