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Modern Compressible Flow: With Historical Perspective

Taschenbuch von John Anderson

91987146

nur 72,09 €

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  • Details
  • Beschreibung
  • Inhaltsverzeichnis
Details
Artikel-Nr.:
91987146
Im Sortiment seit:
25.02.2020
Erscheinungsdatum:
11.02.2020
Medium:
Taschenbuch
Einband:
Kartoniert / Broschiert
Auflage:
4. Auflage von 1920
4. Auflage
Autor:
Anderson, John
Verlag:
McGraw-Hill Education Ltd
Imprint:
McGraw-Hill Education
Sprache:
Englisch
Rubrik:
Luftfahrt-
Raumfahrttechnik
Gewicht:
1011 gr
Beschreibung
The response to the first three editions of Modern Compressible Flow: With Historical Perspective , from students, faculty, and practicing professionals has been overwhelmingly favorable. Therefore, this new edition preserves much of this successful content while adding important new components. It preserves the author's informal writing style that talks to the reader, that gains the readers' interest, and makes the study of compressible flow an enjoyable experience. Moreover, it blends the classical nature of the subject with modern aspects of computational fluid dynamics (CFD) and high temperature gas dynamics so important to modern applications of compressible flow. In short, this book is a unique teaching and learning experience.
Inhaltsverzeichnis
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 Appendix C Oblique Shock Properties: y = 1.4