Shock Wave—Turbulence Interactions
By Yiannis Andreopoulos, J. Agui, G. Briassulis. 2000
288 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/c96bd257a0960b68742b65f2f386650a1715897f
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
- Alexander A. Zheltovodov
- M. Loginov
- D. O. Astronomy
- Lian-Ping Wang
- Nikolaus A. Adams
- John A. Center
- Bruce G. Elmegreen
- U. Texas
In Computational Mechanics
- Alexander A. Zheltovodov
- M. Loginov
- Nikolaus A. Adams
- D. O. Astronomy
- Lian-Ping Wang
- Shiyi Chen
- John A. Center
- Yipeng Shi
Citations in the corpus
- Effects of upstream boundary layer on the unsteadiness of shock-induced separation (2006, unknown): “This phenomenon of amplification of turbulent fluctuations behind a shock has been observed in both numerical and experimental studies (Andreopoulos et al. 2000; Agui 1998; Lee, Lele & Moin 1993; Loginov, Adams & Zheltovodov 2004).”
- Advances in CFD prediction of shock wave turbulent boundary layer interactions (2003, unknown): “[21] Andreopoulos Y, Agui H, Briassulis G.”
- Large-eddy simulation of shock-wave/turbulent-boundary-layer interaction (2006, background): “The observed phenomenon provides evidence for an additional mechanism which enhances the level of turbulent fluctuations in this flow region along with direct interaction of shocks and turbulence (Andreopoulos et al. 2000; Anyiwo & Bushnell 1982).”
- Interstellar Turbulence I: Observations and Processes (2004, background): “…supersonic turbulence, a relation like this makes sense because the densest regions have been decelerated behind shock fronts, although shocks propagating in a turbulent medium can increase the velocity dispersion behind them (Rotman 1991, Andreopoulos et al. 2000), which gives the opposite effect.”
- Effect of compressibility on the small-scale structures in isotropic turbulence (2012, background): “…components, the solenoidal dissipation s = (µ/Re)ωiωi, the dilatational dissipation c = (4/3)(µ/Re)θ 2, and the mixed term m = (2µ/Re)((∂ui/∂xj)(∂uj/∂xi) − θ 2), which represents the contributions to the dissipation rate by the purely non-homogeneous part of the flow (Andreopoulos et al. 2000).”
- Rotating detonation wave propulsion: Experimental challenges, modeling, and engine concepts (2014, unknown): “This study can be viewed as the reactive analog of more extensive studies of shock–turbulence interactions [63,64].”