Large-Eddy Simulation of Boundary Layer Transition on Swept Wings
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[1] M. Gaster,et al. A Simple Device for Preventing Turbulent Contamination on Swept Leading Edges , 1965, The Journal of the Royal Aeronautical Society.
[2] H. Bippes,et al. Experimental Study of Instability Modes in a Three-dimensional Boundary Layer. , 1987 .
[3] Craig L. Streett,et al. Spectral multi-domain for large-scale fluid dynamic simulations , 1989 .
[4] W. Saric,et al. Crossflow-vortex instability and transition on a 45 deg swept wing , 1989 .
[5] P. Moin,et al. A dynamic subgrid‐scale eddy viscosity model , 1990 .
[6] P. R. Spalart,et al. Direct Numerical Study of Crossflow Instability , 1990 .
[7] William S. Saric,et al. A high-frequency, secondary instability of crossflow vortices that leads to transition , 1991 .
[8] D. Lilly,et al. A proposed modification of the Germano subgrid‐scale closure method , 1992 .
[9] Ronald D. Joslin,et al. The role of stationary cross‐flow vortices in boundary‐layer transition on swept wings , 1994 .