Characteristics Finite Element Methods in Computational Fluid Dynamics

Name: Characteristics Finite Element Methods in Computational Fluid Dynamics
Brand: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG
SKU: 9783642064302
Price: 849.15 PLN
Availability: InStock

Autor: Joe Iannelli

Język:

Oprawa: Miękka

Wydawca: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG

Dostępność: Dostępna u dostawcy

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This book details a systematic characteristics-based finite element procedure to investigate incompr...

Informacje o książce

Autor

Joe Iannelli

Język

Angielski

Oprawa

Książka - Miękka

Data wydania

2010

strony

730

EAN

9783642064302

ISBN

3642064302

Enbook ID

01651682

Wydawca

Springer-Verlag Berlin and Heidelberg GmbH & Co. KG

Waga

1139

Wymiary

155 x 235 x 41

Pełny opis

This book details a systematic characteristics-based finite element procedure to investigate incompressible, free-surface and compressible flows. Several sections derive the Fluid Dynamics equations from first thermo-mechanics principles and develop this multi-dimensional and infinite-directional upstream procedure by combining a finite element discretization with an implicit non-linearly stable Runge-Kutta time integration for the numerical solution of the Euler and Navier Stokes equations.This book details a systematic characteristics-based finite element procedure to investigate incompressible, free-surface and compressible flows. The fluid dynamics equations are derived from basic thermo-mechanical principles and the multi-dimensional and infinite-directional upstream procedure is developed by combining a finite element discretization of a characteristics-bias system with an implicit Runge-Kutta time integration. For the computational solution of the Euler and Navier Stokes equations, the procedure relies on the mathematics and physics of multi-dimensional characteristics. As a result, the procedure crisply captures contact discontinuities, normal as well as oblique shocks, and generates essentially non-oscillatory solutions for incompressible, subsonic, transonic, supersonic, and hypersonic inviscid and viscous flows.

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