On the Basic Equations for the Second Order Modeling of Compressible Turbulence

On the Basic Equations for the Second Order Modeling of Compressible Turbulence
Author: National Aeronautics and Space Administration (NASA)
Publsiher: Createspace Independent Publishing Platform
Total Pages: 28
Release: 2018-07-09
Genre: Electronic Book
ISBN: 1722453133

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Equations for the mean and turbulent quantities for compressible turbulent flows are derived. Both the conventional Reynolds average and the mass-weighted, Favre average were employed to decompose the flow variable into a mean and a turbulent quality. These equations are to be used later in developing second order Reynolds stress models for high speed compressible flows. A few recent advances in modeling some of the terms in the equations due to compressibility effects are also summarized. Liou, W. W. and Shih, T.-H. Glenn Research Center NASA ORDER C-99066-G; RTOP 505-62-21...

On the Basic Equations for the Second order Modeling of Compressible Turbulence

On the Basic Equations for the Second order Modeling of Compressible Turbulence
Author: W. W. Liou
Publsiher: Unknown
Total Pages: 30
Release: 1991
Genre: Turbulence
ISBN: UIUC:30112059174232

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author: Anonim
Publsiher: Unknown
Total Pages: 508
Release: 1995
Genre: Aeronautics
ISBN: UVA:X004872569

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Institute for Computational Mechanics in Propulsion ICOMP

Institute for Computational Mechanics in Propulsion  ICOMP
Author: Charles E. Feiler
Publsiher: Unknown
Total Pages: 56
Release: 1992
Genre: Electronic Book
ISBN: NASA:31769000600729

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Center for Modeling of Turbulence and Transition CMOTT

Center for Modeling of Turbulence and Transition  CMOTT
Author: Anonim
Publsiher: Unknown
Total Pages: 172
Release: 1991
Genre: Turbulence
ISBN: UIUC:30112059174216

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Navier Stokes Computation of Compressible Turbulent Flows with a Second Order Closure

Navier Stokes Computation of Compressible Turbulent Flows with a Second Order Closure
Author: National Aeronautics and Space Adm Nasa
Publsiher: Unknown
Total Pages: 70
Release: 2018-11-03
Genre: Electronic Book
ISBN: 1730800475

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A second order closure turbulence model for compressible flows is developed and implemented in a 2D Reynolds-averaged Navier-Stokes solver. From the beginning where a kappa-epsilon turbulence model was implemented in the bidiagonal implicit method of MACCORMACK (referred to as the MAC3 code) to the final stage of implementing a full second order closure in the efficient line Gauss-Seidel algorithm, numerous work was done, individually and collectively. Besides the collaboration itself, the final product of this work is a second order closure derived from the Launder, Reece, and Rodi model to account for near wall effects, which has been called FRAME model, which stands for FRench-AMerican-Effort. During the reporting period, two different problems were worked out. The first was to provide Ames researchers with a reliable compressible boundary layer code including a wide collection of turbulence models for quick testing of new terms, both in two equations and in second order closure (LRR and FRAME). The second topic was to complete the implementation of the FRAME model in the MAC5 code. The work related to these two different contributions is reported. dilatation in presence of stron shocks. This work, which has been conducted during a work at the Center for Turbulence Research with Zeman aimed also to cros-check earlier assumptions by Rubesin and Vandromme. Haminh, Hieu and Kollmann, Wolfgang and Vandromme, Dany Unspecified Center...

Monthly Catalogue United States Public Documents

Monthly Catalogue  United States Public Documents
Author: Anonim
Publsiher: Unknown
Total Pages: 982
Release: 1992
Genre: Government publications
ISBN: UIUC:30112063914714

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications
Author: Anonim
Publsiher: Unknown
Total Pages: 1734
Release: 1992
Genre: Government publications
ISBN: MINN:31951P00237274B

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