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Theoretical and Applied ­Aerodynamics
And Related Numerical Methods

Rating
Format
Hardback, 620 pages
Published
Netherlands, 1 April 2015

This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including:

-The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings.

- The linearized theories for compressible subsonic and supersonic aerodynamics.

- The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained.

- Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations.

There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows.

A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.



J.J. Chattot, University of California, Davis, Dept. Mechanical & Aeronautical, Davis, USA M.M. Hafez,  University of California, Davis, Dept. Mechanical & Aeronautical, Davis, USA.

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£85.88
Ships from UK Estimated delivery date: 11th Feb - 13th Feb from UK

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Product Description

This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including:

-The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings.

- The linearized theories for compressible subsonic and supersonic aerodynamics.

- The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained.

- Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations.

There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows.

A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.



J.J. Chattot, University of California, Davis, Dept. Mechanical & Aeronautical, Davis, USA M.M. Hafez,  University of California, Davis, Dept. Mechanical & Aeronautical, Davis, USA.

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Product Details
EAN
9789401798242
ISBN
9401798249
Publisher
Other Information
141 Illustrations, color; 184 Illustrations, black and white; XXI, 620 p. 325 illus., 141 illus. in color.
Dimensions
23.4 x 15.6 x 3.5 centimeters (1.04 kg)

Table of Contents

Part I Fundamental Aerodynamics.- Introduction.- Inviscid, Incompressible Flow Past Circular Cylinders and Joukowski Airfoils.- Inviscid, Incompressible Flow Past Thin Airfoils.- Inviscid, Compressible Flow Past Thin Airfoils.- Inviscid, Unsteady Flows past Airfoils.- Flow Past Large and Moderate Aspect Ratio Wings.- Axisymmetric Flows and Slender Body Theories.- Viscous Fluid Flow and Laminar Boundary Layers.- Viscous/Inviscid Interaction Procedures.- Part II Special Topics.- Wind Turbine and Propeller Aerodynamics – Analysis and Design.- Glider and Airplane Design.- Introduction to Hypersonic Flows.- Flow Analogies.- Part III Problems and Solutions.- Problems.- Solutions to Problems Appendix: Special Techniques.

Promotional Information

"The book is a masterpiece for aerodynamics of analytical and numerical techniques. ... To me it is clear that this book can be either a basic textbook for a graduate course or an additional reference for a course focused more on computational fluid dynamics, or traditional fluid mechanics. It is also an invaluable handbook of special solutions for engineers." (Prof. emeritus Olivier Pironneau, University Pierre et Marie Curie, Paris, Member of the 'Academie des Sciences')

About the Author

J.J. Chattot, University of California, Davis, Dept. Mechanical & Aeronautical, Davis, USA
M.M. Hafez,  University of California, Davis, Dept. Mechanical & Aeronautical, Davis, USA.

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