1. N. Hildebrand, A. Dwivedi, P. Shrestha, J. W. Nichols, M. R. Jovanovic, and G. V. Candler. Sensitivity analysis for the control of oblique shock/boundary layer interactions at Mach 5.92. In Proceedings of the 47th AIAA Fluid Dynamics Conference, Denver, CO, 2017. Note: To appear. Keyword(s): Adjoint equations, Base-flow sensitivity, Direct numerical simulations, Global stability analysis, Flow modeling and control, Hypersonic flows, Transition to turbulence. [bibtex-entry]



2. P. Shrestha, A. Dwivedi, N. Hildebrand, J. W. Nichols, M. R. Jovanovic, and G. V. Candler. Interaction of an oblique shock with a transitional Mach 5.65 boundary layer. In Proceedings of the 46th AIAA Fluid Dynamics Conference, Washington, DC, 2016. Keyword(s): Direct numerical simulations, Dynamic mode decomposition, Flow modeling and control, Hypersonic flows, Transition to turbulence. [bibtex-entry]

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