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Modern compressible flow : with historical perspective

Author: John David Anderson
Publisher: Boston : McGraw-Hill, 200.
Series: McGraw-Hill series in aeronautical and aerospace engineering.
Edition/Format:   Book : English : 3rd. ed. ;international edView all editions and formats
Database:WorldCat
Summary:

Provides an accessible approach to compressible flow useful for Mechanical and Aerospace Engineering students. This book uses many historical vignettes that show the evolution of the field. It also  Read more...

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Document Type: Book
All Authors / Contributors: John David Anderson
ISBN: 0071241361 9780071241366
OCLC Number: 71626491
Description: xvi, 760 p. : ill. ; 25 cm.
Contents: 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
Series Title: McGraw-Hill series in aeronautical and aerospace engineering.
Responsibility: John D. Anderson, Jr.

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