Analysis of low speed unsteady airfoil flows ; with 3 tables, and a CD-ROM

The authors take the view that a full understanding of the physics of lift generation is possible only by considering the unsteady aerodynamics of the starting vortex generation process. This view is also reflected in the methods of computational fluid dynamics when accurate steady-state solutions can be obtained by solving unsteady flow equations. This comprehensive textbook concentrates on unsteady low-speed flows over airfoils restricting the discussions to two-dimensional incompressible flows. The first chapter describes the physics of unsteady flow mechanisms for the generation of lift and of thrust on flapping wings. Then the Navier-Stokes equations and their Reynolds-averaged form are presented. The bulk of the book is devoted to three methods for the computation of steady and unsteady airfoil flows based on the so-called panel method pioneered by the senior author of this book. Many applications of practical importance in industry are given and the computer programs together with their accompanying CD-Roms are carefully documented. TOC:Physics of Unsteady Flows.- The Differential Equations of Fluid Flow.- Panel Methods.- Applications of Panel Method.- Boundary-Layer Methods.- Applications of Boundary-Layer Methods: Flows Without Separation.- Applications of Boundary-Layer Methods: Flows With Separation.- Navier-Stokes Methods.- Applications of Navier-Stokes Methods.- Applications of Navier-Stokes Methods.

Standort
Deutsche Nationalbibliothek Frankfurt am Main
ISBN
9780966846188
0966846184
9783540229322
3540229329
Maße
25 cm
Umfang
XII, 226 S.
Sprache
Englisch
Anmerkungen
graph. Darst.

Klassifikation
Ingenieurwissenschaften und Maschinenbau
Schlagwort
Tragflügelumströmung
Instationäre Strömung
Numerische Strömungssimulation

Ereignis
Veröffentlichung
(wo)
Long Beach, Calofornia, Heidelberg, Berlin, Heidelberg, New York
(wer)
Horizons Publ., Springer
(wann)
2005
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11.06.2025, 13:49 MESZ

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  • 2005

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