Produktdetaljer
Biographical note
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 1986–1987, 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.The 6th edition of Fundamentals of Aerodynamics is meant to be read. The writing style is intentionally conversational in order to make the book easier to read. The book is designed to talk to the reader; in part to be a self-teaching instrument. Learning objectives have been added to each chapter to reflect what is believed to be the most important items to learn from that particular chapter. The 6th edition emphasizes the rich theoretical and physical background of aerodynamics, and marbles in many historical notes to provide a background as to where the aerodynamic technology comes from. Also new with this edition, are Integrated Work Challenges that pertain to the chapter as a whole, and give the reader the opportunity to integrate the material in that chapter in order to solve a "bigger picture".
Now available with the sixth edition of Fundamentals of Aerodynamics, Connect. Connect is the only integrated learning system that empowers students by continuously adapting to deliver precisely what they need, when they need it, how they need it, so that your class time is more engaging and effective. Within Connect, SmartBook is available with the 6th edition as well. SmartBook is the first and only adaptive eBook for the Higher Education market. SmartBook facilitates the reading process by using practice questions to identify what content a student knows and doesn't know. As a student reads the text, the material continuously adapts to ensure that he or she is focused on the content most crucial to closing specific knowledge gaps.
Part One - Fundamental Principles
1) Aerodynamics: Some Introductory Thoughts
2) Aerodynamics: Some Fundamental Principles and Equations
Part Two - 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 Three - 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 Four - Viscous Flow
15) Introduction to the Fundamental Principles and Equations of Viscous Flow
16) Some Special Cases; Couette and Poiseuille Flows
17) Introduction to Boundary Layers
18) Laminar Boundary Layers
19) Turbulent Boundary Layers
20) Navier-Stokes Solutions: Some Examples
Appendix A - Isentropic FlowProperties
Appendix B - Normal Shock Properties
Appendix C - Prandtl-Meyer Function and Mach Angle
Appendix D - Standard Atmosphere, SI Units
Appendix E - Standard Atmosphere, English Engineering Units