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03589nam a22005655i 4500 |
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978-3-540-45343-7 |
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20151204163551.0 |
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100301s2006 gw | s |||| 0|eng d |
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|a 9783540453437
|9 978-3-540-45343-7
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|a 10.1007/978-3-540-45343-7
|2 doi
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|a QC6.4.C6
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|a PHD
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|a SCI041000
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|a 531
|2 23
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|a Iannelli, Joe.
|e author.
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|a Characteristics Finite Element Methods in Computational Fluid Dynamics
|h [electronic resource] /
|c by Joe Iannelli.
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|a Berlin, Heidelberg :
|b Springer Berlin Heidelberg,
|c 2006.
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300 |
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|a XXVI, 730 p.
|b online resource.
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|a text
|b txt
|2 rdacontent
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|a computer
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|2 rdamedia
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|a online resource
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|a text file
|b PDF
|2 rda
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|a Computational Fluid and Solid Mechanics,
|x 1860-482X
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|a Governing Equations of Fluid Mechanics -- Constitutive and State Equations -- State Equations for Reacting Air -- Euler and Navier Stokes Systems -- Quasi One-Dimensional and Free-Surface Equations -- Overview of CFD Algorithm Development -- The Finite Element Method -- Non-Linearly Stable Implicit Runge-Kutta Time Integrations -- One-Dimensional Non-Discrete Characteristics-Bias Resolution -- Characteristics-Bias Controller and Length -- Computational Analysis of Quasi-1-D Incompressible Flows -- Numerical Study of Generalized Quasi-1-D Free Surface Flows -- CFD Investigation of Generalized Quasi-1-D Compressible Flows -- Multi-Dimensional Characteristics and Characteristics-Bias Systems -- Multi-Dimensional Incompressible Flows -- Multi-Dimensional Free-Surface Flows -- Multi-Dimensional Compressible Flows.
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|a 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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650 |
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|a Physics.
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|a Computer mathematics.
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|a Continuum physics.
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|a Fluids.
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|a Applied mathematics.
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|a Engineering mathematics.
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|a Computational intelligence.
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|a Fluid mechanics.
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|a Physics.
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|a Classical Continuum Physics.
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|a Engineering Fluid Dynamics.
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|a Appl.Mathematics/Computational Methods of Engineering.
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|a Computational Science and Engineering.
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|a Fluid- and Aerodynamics.
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650 |
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|a Computational Intelligence.
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710 |
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|a SpringerLink (Online service)
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|t Springer eBooks
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776 |
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|i Printed edition:
|z 9783540251811
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830 |
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|a Computational Fluid and Solid Mechanics,
|x 1860-482X
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856 |
4 |
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|u http://dx.doi.org/10.1007/978-3-540-45343-7
|z Full Text via HEAL-Link
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912 |
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|a ZDB-2-ENG
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950 |
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|a Engineering (Springer-11647)
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