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A Point Implicit Unstructured Grid Solver for the Euler and Navier-Stokes Equations

A Point Implicit Unstructured Grid Solver for the Euler and Navier-Stokes Equations PDF Author: J.R. Stewart
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


A Point Implicit Unstructured Grid Solver for the Euler and Navier-Stokes Equations

A Point Implicit Unstructured Grid Solver for the Euler and Navier-Stokes Equations PDF Author: J.R. Stewart
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Implicit, Pressure-based Incompressible Navier-Stokes Equations Solver for Unstructured Meshes

Implicit, Pressure-based Incompressible Navier-Stokes Equations Solver for Unstructured Meshes PDF Author: Yu Jiang
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 324

Book Description


The Finite Element Method Set

The Finite Element Method Set PDF Author: O. C. Zienkiewicz
Publisher: Elsevier
ISBN: 0080531679
Category : Technology & Engineering
Languages : en
Pages : 1863

Book Description
The sixth editions of these seminal books deliver the most up to date and comprehensive reference yet on the finite element method for all engineers and mathematicians. Renowned for their scope, range and authority, the new editions have been significantly developed in terms of both contents and scope. Each book is now complete in its own right and provides self-contained reference; used together they provide a formidable resource covering the theory and the application of the universally used FEM. Written by the leading professors in their fields, the three books cover the basis of the method, its application to solid mechanics and to fluid dynamics. * This is THE classic finite element method set, by two the subject's leading authors * FEM is a constantly developing subject, and any professional or student of engineering involved in understanding the computational modelling of physical systems will inevitably use the techniques in these books * Fully up-to-date; ideal for teaching and reference

The finite element method in the 1990’s

The finite element method in the 1990’s PDF Author: Eugenio Onate
Publisher: Springer Science & Business Media
ISBN: 3662103265
Category : Technology & Engineering
Languages : en
Pages : 632

Book Description
Edited on the occasion of Prof. Olgierd C. Zienkiewicz' 70th birthday, this book contains original contributions from eminent scientists dealing with a wide range of theoretical aspects of the Finite Element Method and its application to a variety of engineering problems. The book provides an overview of the state-of-the-art of finite element technology in the last decade of the 20th century.

The Finite Element Method for Fluid Dynamics

The Finite Element Method for Fluid Dynamics PDF Author: Olek C Zienkiewicz
Publisher: Butterworth-Heinemann
ISBN: 0080951376
Category : Technology & Engineering
Languages : en
Pages : 581

Book Description
The Finite Element Method for Fluid Dynamics offers a complete introduction the application of the finite element method to fluid mechanics. The book begins with a useful summary of all relevant partial differential equations before moving on to discuss convection stabilization procedures, steady and transient state equations, and numerical solution of fluid dynamic equations. The character-based split (CBS) scheme is introduced and discussed in detail, followed by thorough coverage of incompressible and compressible fluid dynamics, flow through porous media, shallow water flow, and the numerical treatment of long and short waves. Updated throughout, this new edition includes new chapters on: Fluid-structure interaction, including discussion of one-dimensional and multidimensional problems Biofluid dynamics, covering flow throughout the human arterial system Focusing on the core knowledge, mathematical and analytical tools needed for successful computational fluid dynamics (CFD), The Finite Element Method for Fluid Dynamics is the authoritative introduction of choice for graduate level students, researchers and professional engineers. A proven keystone reference in the library of any engineer needing to understand and apply the finite element method to fluid mechanics Founded by an influential pioneer in the field and updated in this seventh edition by leading academics who worked closely with Olgierd C. Zienkiewicz Features new chapters on fluid-structure interaction and biofluid dynamics, including coverage of one-dimensional flow in flexible pipes and challenges in modeling systemic arterial circulation

Preconditioned Implicit Solvers for the Navier-Stokes Equations on Distributed-memory Machines

Preconditioned Implicit Solvers for the Navier-Stokes Equations on Distributed-memory Machines PDF Author: Kumud Ajmani
Publisher:
ISBN:
Category : Navier-Stokes equations
Languages : en
Pages : 16

Book Description


An Examination of Several High Resolution Schemes Applied to Complex Problems in High Speed Flows

An Examination of Several High Resolution Schemes Applied to Complex Problems in High Speed Flows PDF Author: Norbert Kroll
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 68

Book Description
A comparative study of five upwind schemes was performed to evaluate their ability accurately model the convective fluxes of the Euler equations for problems containing complex shock structure. The schemes investigated used a variety of Reimann solvers and obtained higher order accuracy using either a MUSCL or non-MUSCL approach. The MUSCL-type schemes included the flux vector split formulations of Steiger-Warming and van Leer and the flux difference split approach of Roe. The Non-MUSCL schemes included the Symmetric and Upwind TVD methods of Yee, and Harten and Yee. Two central difference schemes provide a basis for the evaluation of these upwind methods. The comparison was performed using identical meshes and convergence criteria. In a supersonic blunt body flow, all the upwind schemes displayed comparably resolved bow shocks, independent of free stream Mach number. However, a complex type IV shock on cowl lip example pointed out significant difference in the accuracy and convergence behavior of the schemes. A comparison of the flow structure shown by the various algorithms on identical grids indicated that the discrete solutions obtained with Upwind TVD and Roe flux difference splitting were the least diffusive of the upwind methods considered.

A Fast Implicit Upwind Solution Algorithm for Three-dimensional Unstructured Dynamic Meshes

A Fast Implicit Upwind Solution Algorithm for Three-dimensional Unstructured Dynamic Meshes PDF Author: John T. Batina
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

Book Description


Hypersonic Flows for Reentry Problems

Hypersonic Flows for Reentry Problems PDF Author: Jean-Antoine Desideri
Publisher: Springer Science & Business Media
ISBN: 3642765270
Category : Science
Languages : en
Pages : 1231

Book Description
This entry describes the experimental work conducted in the Department of Aeronautics at Imperial College in connection with Test Problems 1 and 2 of the "Workshop on Hypersonic Flows for Reentry Problems, Part I". These are defined as follows: Test Problem 1 Flow Over a Slender Cone Test Problem 2 Turbulent Base Flow The main requirement of this text is to present the experimental data for direct comparison with the predictions of CFD codes. We have therefore concentrated mainly on a factual statement of measuring techniques and results, together with an assessment of experimental accuracy. Future publications will be devoted to more extensive physical interpretations and discussions of the results. We have produced a large volume of data, some of which were categorised as "MANDATORY" and some as "OPTIONAL" for the purposes of CFD validation. However, only the "MANDATORY" data are presented here, although the other data are available and will be published separately later. 2. EXPERIMENTAL ARRANGEMENT 2. 1 The Test Facility The experiments were conducted in the Imperial College No. 2 Gun tunnel. This facility is a conventional intermittent blowdown tunnel with a contoured Mach 9 (nominal) axisymmetric nozzle fed by a free piston compression heater. The operating condition under which the data contained in this report were obtained is presented in Table 1. Test 2 T (oK) M b. Mlm Po (N/m ) Re/m T (oK) IX) IX) Case IX) w 1. 1 7 7 +0. 14 9. 16 6. 67x10 5. 5xl0 59.