The approximate deconvolution model for large-eddy simulations of compressible flows and its application to shock-turbulent-boundary-layer interaction

By S. Stolz, Nikolaus A. Adams, L. Kleiser. 2001

276 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/826b60d292e99646020a299fc5dcf013fbc7eb1d

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Alexander A. Zheltovodov
2. M. Loginov
3. A. Panaras
4. Hong Yan
5. Doyle D. Knight
6. Nikolaus A. Adams
7. Joel H. Ferziger
8. Robert L. Street

In Computational Mechanics

1. Alexander A. Zheltovodov
2. M. Loginov
3. Nikolaus A. Adams
4. Robert L. Street
5. A. Panaras
6. Doyle D. Knight
7. Hong Yan
8. Joel H. Ferziger

Citations in the corpus

• Large-eddy simulation of shock-wave/turbulent-boundary-layer interaction (2006, methodology): “The relaxation parameter χ is estimated dynamically Stolz et al. (2001a).”
• Advances in CFD prediction of shock wave turbulent boundary layer interactions (2003, background): “Table 5: Details of Computations Reference Type Grid SA TA Adams[90, 91, 44] DNS 1000×180×80 5th 3rd Rizzetta et al[92] DNS 421×151×81 6th 2nd LES-S 421×151×81 6th 2nd LES-D 421×151×81 6th 2nd Stolz et al [93] LES 334× 91× 31 6th 3rd Advances in CFD Prediction of Shock Wave Turbulent Boundary Layer ”
• Explicit Filtering and Reconstruction Turbulence Modeling for Large-Eddy Simulation of Neutral Boundary Layer Flow (2005, background): “Their scale-similarity properties have desirable effects in a priori tests (Katopodes et al. 2000b; Stolz et al. 1999).”