Wall-Modeled LES of Flow over a Gaussian Bump with Strong Pressure Gradients and Separation-Reference-Cited by-同舟云学术

Wall-Modeled LES of Flow over a Gaussian Bump with Strong Pressure Gradients and Separation

Published:2020-06-08 Issue: Volume: Page:
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Container-title:AIAA AVIATION 2020 FORUM
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Author:

Balin Riccardo¹,Jansen Kenneth E.¹,Spalart Philippe R.²

Affiliation:

1. University of Colorado, Boulder

2. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Reference49 articles.

1. Grid-point requirements for large eddy simulation: Chapman’s estimates revisited

2. WALL-LAYER MODELS FOR LARGE-EDDY SIMULATIONS

3. Large-Eddy and Direct Numerical Simulations of the Bachalo-Johnson Flow with Shock-Induced Separation

4. An improved dynamic non-equilibrium wall-model for large eddy simulation

5. Lehmkuhl, O., Park, G. I., and Moin, P. “LES of flow over the NASA Common Research Model with near-wall modeling,” Center for Turbulence Research Annual Research Briefs 2016, 2016, pp.335-341.

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