1. A. Dwivedi. Global input-output analysis of flow instabilities in high-speed compressible flows. PhD thesis, University of Minnesota, 2020. Keyword(s): Adjoint equations, Base-flow sensitivity, Compressible flows, Compression ramp flow, Direct numerical simulations, Energy amplification, Flow modeling and control, Global stability analysis, Hypersonic flows, Input-output analysis, Shock Boundary layer interaction, Reattachment vortices, Transient growth, Transition to turbulence. [bibtex-entry]

1. A. Dwivedi, N. Hildebrand, J. W. Nichols, G. V. Candler, and M. R. Jovanovic. Transient growth analysis of oblique shock wave/boundary-layer interactions at Mach 5.92. Phys. Rev. Fluids, 5(6):063904 (20 pages), June 2020. Keyword(s): Adjoint equations, Base-flow sensitivity, Compressible flows, Direct numerical simulations, Energy amplification, Global stability analysis, Flow modeling and control, Hypersonic flows, Transient growth, Transition to turbulence. [bibtex-entry]



2. N. Hildebrand, A. Dwivedi, J. W. Nichols, M. R. Jovanovic, and G. V. Candler. Simulation and stability analysis of oblique shock wave/boundary layer interactions at Mach 5.92. Phys. Rev. Fluids, 3(1):013906 (23 pages), January 2018. Keyword(s): Adjoint equations, Base-flow sensitivity, Compressible flows, Direct numerical simulations, Global stability analysis, Flow modeling and control, Hypersonic flows, Transition to turbulence. [bibtex-entry]

1. N. Hildebrand, A. Dwivedi, G. S. Sidharth, J. W. Nichols, M. R. Jovanovic, and G. V. Candler. Instabilities in laminar shock boundary layer interactions. In Proceedings of the 2019 IUTAM Symposium on Laminar-Turbulent Transition, London, United Kingdom, 2019. Keyword(s): Adjoint equations, Base-flow sensitivity, Compressible flows, Direct numerical simulations, Global stability analysis, Flow modeling and control, Hypersonic flows, Transition to turbulence. [bibtex-entry]



2. N. Hildebrand, A. Dwivedi, J. W. Nichols, G. V. Candler, and M. R. Jovanovic. Sensitivity analysis for the control of oblique shock wave/laminar boundary layer interactions at Mach $5.92$. In Proceedings of the 47th AIAA Fluid Dynamics Conference, Denver, CO, pages 4312 (14 pages), 2017. Keyword(s): Adjoint equations, Base-flow sensitivity, Compressible flows, Direct numerical simulations, Global stability analysis, Flow modeling and control, Hypersonic flows, Transition to turbulence. [bibtex-entry]

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