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. A. Dwivedi, G. S. Sidharth, J. W. Nichols, G. V. Candler, and M. R. Jovanovic. Reattachment vortices in hypersonic compression ramp flow: an input-output analysis. J. Fluid Mech., 880:113-135, December 2019. Keyword(s): Compressible flows, Compression ramp flow, Flow modeling and control, Hypersonic flows, Input-Output analysis, Shock Boundary layer interaction, Reattachment vortices, Transition to turbulence. [bibtex-entry]



3. 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. A. Dwivedi, G. V. Candler, and M. R. Jovanovic. A frequency domain analysis of compressible linearized Navier-Stokes equations in a hypersonic compression ramp flow. In Proceedings of the 2020 American Control Conference, Denver, CO, pages 4325-4330, 2020. Keyword(s): Compressible flows, Compression ramp flow, Flow modeling and control, Hypersonic flows, Input-Output analysis, Shock Boundary layer interaction, Reattachment vortices, Transition to turbulence. [bibtex-entry]



2. 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]



3. A. Dwivedi, G. S. Sidharth, G. V. Candler, J. W. Nichols, and M. R. Jovanovic. Input-output analysis of shock boundary layer interaction. In Proceedings of the 48th AIAA Fluid Dynamics Conference, Atlanta, GA, pages 3220 (17 pages), 2018. Keyword(s): Compressible flows, Input-Output analysis, Shock Boundary layer interaction, Hypersonic flows. [bibtex-entry]



4. N. Hildebrand, J. W. Nichols, G. V. Candler, and M. R. Jovanovic. Transient growth in oblique shock wave/laminar boundary layer interactions at Mach 5.92. In Proceedings of the 48th AIAA Fluid Dynamics Conference, Atlanta, GA, pages 3221 (17 pages), 2018. Keyword(s): Adjoints, Compressible flows, Global stability analysis, Hypersonic flows, Transient growth. [bibtex-entry]



5. A. Dwivedi, J. W. Nichols, M. R. Jovanovic, and G. V. Candler. Optimal spatial growth of streaks in oblique shock/boundary layer interaction. In Proceedings of the 47th AIAA Fluid Dynamics Conference, Denver, CO, pages 4163 (17 pages), 2017. Keyword(s): Compressible flows, Direct numerical simulations, Transient growth, Hypersonic flows, Transition to turbulence. [bibtex-entry]



6. 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]



7. P. Shrestha, J. W. Nichols, M. R. Jovanovic, and G. V. Candler. Study of trip-induced hypersonic boundary layer transition. In Proceedings of the 47th AIAA Fluid Dynamics Conference, Denver, CO, pages 4513 (21 pages), 2017. Keyword(s): Direct numerical simulations, Dynamic mode decomposition, Roughness elements, Hypersonic flows, Transition to turbulence. [bibtex-entry]



8. 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, pages 3647 (14 pages), 2016. Keyword(s): Compressible flows, Direct numerical simulations, Dynamic mode decomposition, Flow modeling and control, Hypersonic flows, Transition to turbulence. [bibtex-entry]

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