Modern Compressible Flow: With Historical Perspective

Anderson, John

Brossura

ISBN 10: 0071121617 ISBN 13: 9780071121613

Casa editrice: McGraw-Hill Education, 2002

Anderson's book provides the most accessible approach to compressible flow for Mechanical and Aerospace Engineering students. 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 student-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 in industry & research.A new Book Website will contain all problem solutions for instructors, and extended information on CFD.

L'autore:

John D. Anderson, Jr., was born in Lancaster, Pennsylvania, on October 1, 1937. He attended the University of Florida, graduating in 1959 with high honors and a Bachelor of Aeronautical Engineering Degree. From 1959 to 1962, he was a Lieutenant and Task Scientist at the Aerospace Research Laboratory at Wright-Patterson Air Force Base. From 1962 to 1966, he attended the Ohio State University under the National Science Foundation and NASA Fellowships, graduating with a PhD in Aeronautical and Astronautical Engineering. In 1966, he joined the U.S. Naval Ordnance Laboratory as Chief of the Hypersonics Group. In 1973, he became Chairman of the Department of Aerospace Engineering at the University of Maryland, and since 1980 has been Professor of Aerospace Engineering at the University of Maryland. In 1982, he was designated a Distinguished Scholar/Teacher by the University. During 19861987, while on sabbatical from the University, Dr. Anderson occupied the Charles Lindbergh Chair at the National Air and Space Museum of the Smithsonian Institution. He continued with the Air and Space Museum one day each week as their Special Assistant for Aerodynamics, doing research and writing on the History of Aerodynamics. In addition to his position as Professor of Aerospace Engineering, in 1993, he was made a full faculty member of the Committee for the History and Philosophy of Science and in 1996 an affiliate member of the History Department at the University of Maryland. In 1996, he became the Glenn L. Martin Distinguished Professor for Education in Aerospace Engineering. In 1999, he retired from the University of Maryland and was appointed Professor Emeritus. He is currently the Curator for Aerodynamics at the National Air and Space Museum, Smithsonian Institution.

Contenuti:

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