Evaluation of Explicit Algebraic Reynolds-Stress Models for Separated Supersonic Flows-Reference-Cited by-同舟云学术

Evaluation of Explicit Algebraic Reynolds-Stress Models for Separated Supersonic Flows

Published:1998-01 Issue:1 Volume:36 Page:24-30
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Rizzetta Donald P.¹

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7913

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.370

Reference38 articles.

1. Prediction of complex aerodynamic flows with explicit algebraic stress models

2. A more general effective-viscosity hypothesis

3. Progress in the development of a Reynolds-stress turbulence closure

4. Rodi, W. “The Predictionof Free Turbulent Boundary Layers by Use of a Two-EquationModel of Turbulence,” Ph.D. Thesis, Mechanical Engineering Dept.Imperial College, London,Dec. 1972.

5. On nonlinear K-l and K-ε models of turbulence

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