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Aerodynamics for engineers / John J. Bertin and Russell M. cummings

By: Bertin, John J, 1938-.
Contributor(s): Cummings, Russell M. (Russell Mark).
Publisher: Upper Saddle River, N.J. : Pearson/Prentice Hall, c2009Edition: 5th ed.Description: xx, 732 p. : ill. ; 24 cm.ISBN: 9780132272681 (hbk.).Subject(s): AerodynamicsDDC classification: 629.1323
Contents:
Ch. 1 Why Study Aerodynamics? - Ch. 2 Fundamentals of Fluid Mechanics . - Ch. 3 Dynamics of an Incompressible, Inviscid Flow Field. - Ch. 4 Viscous Boundary Layers. - Ch. 5 Characteristic Parameters for Airfoil and Wing Aerodynamics. - Ch. 6 Incompressible Flows Around Airfoils of Infinite Span. - Ch. 7 Incompressible Flow About Wings of Finite Span. - Ch. 8 Dynamics of a Compressible Flow Field. - Ch. 9 Compressible, Subsonic Flows and Transonic Flows. - Ch. 10 Two-Dimensional, Supersonic Flows Around Thin Airfoils. - Ch. 11 Supersonic Flows over Wings and Airplane Configurations. - Ch. 12 Hypersonic Flows. - Ch. 13 Aerodynamic Design Considerations. - Ch. 14 Tools for Defining the Aerodynamic Environment. - App. A The Equations of Motion Written in Conservation Form. - App. B A Collection of Often Used Tables.
Item type Current location Call number Copy number Status Notes Date due Barcode Remark
Main Collection TU External Storage-LCS
629.1323 BER (Browse shelf) 1 Available SOExx,07015,03,GR 5000089152 Please fill up online form at https://taylorslibrary.taylors.edu.my/services/external_storage1
Main Collection Taylor's Library-TU
629.1323 BER (Browse shelf) 1 Available SOExx,07017,03,GR 5000089360
Main Collection TU External Storage-LCS
629.1323 BER (Browse shelf) 1 Available SOExx,07017,03,CL 5000063225 Please fill up online form at https://taylorslibrary.taylors.edu.my/services/external_storage1

Previous ed.: 2002

Includes bibliographical references and index.

Ch. 1 Why Study Aerodynamics? - Ch. 2 Fundamentals of Fluid Mechanics . - Ch. 3 Dynamics of an Incompressible, Inviscid Flow Field. - Ch. 4 Viscous Boundary Layers. - Ch. 5 Characteristic Parameters for Airfoil and Wing Aerodynamics. - Ch. 6 Incompressible Flows Around Airfoils of Infinite Span. - Ch. 7 Incompressible Flow About Wings of Finite Span. - Ch. 8 Dynamics of a Compressible Flow Field. - Ch. 9 Compressible, Subsonic Flows and Transonic Flows. - Ch. 10 Two-Dimensional, Supersonic Flows Around Thin Airfoils. - Ch. 11 Supersonic Flows over Wings and Airplane Configurations. - Ch. 12 Hypersonic Flows. - Ch. 13 Aerodynamic Design Considerations. - Ch. 14 Tools for Defining the Aerodynamic Environment. - App. A The Equations of Motion Written in Conservation Form. - App. B A Collection of Often Used Tables.