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Titlebook: Numerical Simulation of Compressible Navier-Stokes Flows; A GAMM Workshop Marie Odile Bristeau,Roland Glowinski,Henri Vivian Book 1987 Frie

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书目名称Numerical Simulation of Compressible Navier-Stokes Flows
副标题A GAMM Workshop
编辑Marie Odile Bristeau,Roland Glowinski,Henri Vivian
视频video
丛书名称Notes on Numerical Fluid Mechanics and Multidisciplinary Design
图书封面Titlebook: Numerical Simulation of Compressible Navier-Stokes Flows; A GAMM Workshop Marie Odile Bristeau,Roland Glowinski,Henri Vivian Book 1987 Frie
描述With the advent of super computers during the last ten years, the numerical simulation of viscous fluid flows modeled by the Navier-Stokes equations is becoming a most useful tool in Aircraft and Engine Design. In fact, compressible Navier-Stokes solvers tend to constitute the basic tools for many industrial applications occuring in the simulation of very complex turbulent and combustion phenomena. In Aerospace Engineering, as an exemple, their mathematical modelization requires reliable and robust methods for solving very stiff non linear partial differential equations. For the above reasons, it was clear that a workshop on this topic would be of interest for the CFD community in order to compare accuracy and efficiency of Navier-Stokes solvers on selected external and internal flow problems using different numerical approaches. The workshop was held on 4-6 December 1985 at Nice, France and organized by INRIA with the sponsorship of the GAMM Committee on Numerical Methods in Fluid Mechanics.
出版日期Book 1987
关键词algorithms; computational fluid dynamics; computer; differential equation; finite element method; fluid m
版次1
doihttps://doi.org/10.1007/978-3-322-87873-1
isbn_softcover978-3-528-08092-1
isbn_ebook978-3-322-87873-1Series ISSN 1612-2909 Series E-ISSN 1860-0824
issn_series 1612-2909
copyrightFriedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig 1987
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Solution of the Compressible Navier-Stokes Equations for a Double Throat Nozzle,w through a double throat nozzle. The accuracy and robustness of the method are shown by the accurate predictions of: extent of recirculation regions; effects of the Reynolds number on the shock structure; the viscous-inviscid interaction. The dependency of the solution upon grid refinement and wall boundary condition is also studied.
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Solution of 2.D Compressible Navier-Stokes Equations for a Double Throat Nozzle by Means of Implicibased on an implicit finite-volume method to solve the unsteady Navier-Stokes equations in a boundary conforming curvilinear coordinate system and to obtain the desired time asymptotic steady state solution. This method has already been successfully developed in 3.D and 2.D axisymmetric cases [1, 5].
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Numerical Simulation of Compressible Navier-Stokes Flow in A Double Throat Nozzle,ormed by using an existing working code, which uses MacCormack’s explicit finite difference scheme. There were no special modifications made in the code for this particular application. The computations were performed on a Cyber 84 5 computer and a CRAY XMP-48 computer using three different grid sizes.
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Presentation of Problems and Discussion of Results,The workshop was organized with the specific purpose to bring together a small number of scientists highly concerned with the numerical solution of the compressible Navier-Stokes equations.
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Experimental Flowfields around NACA 0012 Airfoils Located in Subsonic and Supersonic Rarefied Air SDuring the past decade, significant progress has been achieved in the development of numerical methods, increasing the possibility of aerodynamic calculations. These methods are a valuable tool for everyone who tries to understand specific problems or wants to develop new projects.
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