Fundamentals of Aerodynamics

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.

Part 1 Fundamental Principles1 Aerodynamics: Some Introductory Thoughts2 Aerodynamics: Some Fundamental Principles and EquationsPart 2 Inviscid, Incompressible Flow3 Fundamentals of Inviscid, Incompressible Flow4 Incompressible Flow over Airfoils5 Incompressible Flow over Finite Wings6 Three-Dimensional Incompressible FlowPart 3 Inviscid, Compressible Flow7 Compressible Flow: Some Preliminary Aspects8 Normal Shock Waves and Related Topics9 Oblique Shock and Expansion Waves10 Compressible Flow Through Nozzles, Diffusers, and Wind Tunnels11 Subsonic Compressible Flow over Airfoils: Linear Theory12 Linearized Supersonic Flow13 Introduction to Numerical Techniques for Nonlinear Supersonic Flow14 Elements of Hypersonic FlowPart 4 Viscous Flow15 Introduction to the Fundamental Principles and Equations of Viscous Flow16 Some Special Cases; Couette and Poiseuille Flows17 Introduction to Boundary Layers18 Laminar Boundary Layers19 Turbulent Boundary Layers20 Navier-Stokes Solutions: Some ExamplesAppendix A Isentropic Flow PropertiesAppendix B Normal Shock PropertiesAppendix C Prandtl-Meyer Function and Mach AngleAppendix D Standard Atmosphere, SI UnitsAppendix E Standard Atmosphere, English Engineering Units