Theoretical and Applied Aerodynamics: and Related Numerical Methods
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.

1121202001
Theoretical and Applied Aerodynamics: and Related Numerical Methods
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.

109.99 In Stock
Theoretical and Applied Aerodynamics: and Related Numerical Methods

Theoretical and Applied Aerodynamics: and Related Numerical Methods

by J. J. Chattot, M. M. Hafez
Theoretical and Applied Aerodynamics: and Related Numerical Methods

Theoretical and Applied Aerodynamics: and Related Numerical Methods

by J. J. Chattot, M. M. Hafez

Hardcover(2015)

$109.99 
  • SHIP THIS ITEM
    In stock. Ships in 1-2 days.
  • PICK UP IN STORE

    Your local store may have stock of this item.

Related collections and offers


Overview

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.


Product Details

ISBN-13: 9789401798242
Publisher: Springer Netherlands
Publication date: 04/01/2015
Edition description: 2015
Pages: 620
Product dimensions: 6.10(w) x 9.25(h) x 0.05(d)

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.

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.

What People are Saying About This

From the Publisher

“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 'Académie des Sciences')

From the B&N Reads Blog

Customer Reviews