Fundamentals of aerodynamics - Brossura

Anderson, John

Brossura

ISBN 10: 1259010287 ISBN 13: 9781259010286

Casa editrice: McGraw-Hill Education, 2016

Riassunto

John D. Anderson's textbooks in aeronautical and aerospace engineering have been a cornerstone of McGraw-Hill's success in the engineering discipline for more than two decades. The fifth SI edition of Fundamentals of Aerodynamics continues to offer the most reliable, interesting and up-to-date resources for students and teachers of aerodynamics. Users of past editions will appreciate the continued use of design boxes, historical contents, plentiful worked examples, chapter-opening road maps and other pedagogical features that play a supporting role in Anderson's focus on fundamental concepts. New features: new sections on airplane lift and drag, the blended-wing-body concept, the origin of the swept-wing concept, supersonic flow over cones, hypersonic viscous flow and aerodynamic heating and the design of hypersonic waverider configurations; many additional worked examples and homework problems to provide even more key concept practice for students; and shortened and streamlined Part 4, "Viscous Flow".

Su questo libro

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:

New Page 1

TABLE OF CONTENTS

Preface to the Fifth Edition

Part 1: Fundamental Principles
1. Aerodynamics: Some Introductory Thoughts
2. Aerodynamics: Some Fundamental Principles and Equations

Part 2: Inviscid, Incompressible Flow
3. Fundamentals of Inviscid, Incompressible Flow
4. Incompressible Flow Over Airfoils
5. Incompressible Flow Over Finite Wings
6. Three-Dimensional Incompressible Flow

Part 3: Inviscid, Compressible Flow
7. Compressible Flow: Some Preliminary Aspects
8. Normal Shock Waves and Related Topics
9. Oblique Shock and Expansion Waves
10. Compressible Flow Through Nozzles, Diffusers and Wind Tunnels
11. Subsonic Compressible Flow Over Airfoils: Linear Theory
12. Linearized Supersonic Flow
13. Introduction to Numerical Techniques for Nonlinear Supersonic Flow
14. Elements of Hypersonic Flow

Part 4: Viscous Flow
15. Introduction to the Fundamental Principles and Equations of Viscous Flow
16. A Special Case: Couette Flow
17. Introduction to Boundary Layers
18. Laminar Boundary Layers
19. Turbulent Boundary Layers
20. Navier-Stokes Solutions: Some Examples

Appendix A: Isentropic Flow Properties
Appendix B: Normal Shock Properties
Appendix C: Prandtl-Meyer Function and Mach Angle
Appendix D: Standard Atmosphere

Bibliography
Index

Su questa edizione

• Editore: McGraw-Hill Education
• Data di pubblicazione: 2016
• ISBN 10: 1259010287
• ISBN 13: 9781259010286
• Rilegatura: Copertina flessibile
• Numero edizione: 5
• Numero di pagine: 1098