Theoretical and Applied Aerodynamics

and Related Numerical Methods

Nonfiction, Science & Nature, Science, Physics, Mechanics, Technology, Engineering, Mechanical
Cover of the book Theoretical and Applied Aerodynamics by J. J. Chattot, M. M. Hafez, Springer Netherlands
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Author: J. J. Chattot, M. M. Hafez ISBN: 9789401798259
Publisher: Springer Netherlands Publication: March 31, 2015
Imprint: Springer Language: English
Author: J. J. Chattot, M. M. Hafez
ISBN: 9789401798259
Publisher: Springer Netherlands
Publication: March 31, 2015
Imprint: Springer
Language: English

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.

View on Amazon View on AbeBooks View on Kobo View on B.Depository View on eBay View on Walmart

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.

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