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]



4. J. Jeun, J. W. Nichols, and M. R. Jovanovic. Input-output analysis of high-speed axisymmetric isothermal jet noise. Phys. Fluids, 28(4):047101 (20 pages), April 2016. Note: (Editor's Pick). Keyword(s): Acoustics, Flow modeling and control, Input-output analysis, Jet noise. [bibtex-entry]



5. M. R. Jovanovic, P. J. Schmid, and J. W. Nichols. Sparsity-promoting dynamic mode decomposition. Phys. Fluids, 26(2):024103 (22 pages), February 2014. Keyword(s): Dynamic Mode Decomposition, Flow modeling and control, Convex optimization, Sparsity. [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. 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]



3. 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]



4. 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]



5. 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]



6. W. Ran, A. Zare, J. W. Nichols, and M. R. Jovanovic. The effect of sponge layers on global stability analysis of Blasius boundary layer flow. In Proceedings of the 47th AIAA Fluid Dynamics Conference, Denver, CO, pages 3456 (12 pages), 2017. Keyword(s): Global stability analysis, Sponge layer, Boundary layer flow. [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. J. Jeun, J. W. Nichols, and M. R. Jovanovic. Input-output analysis of heated axisymmetric turbulent jets. In Proceedings of the 22nd AIAA/CEAS Aeroacoustics Conference, Lyon, France, pages 2934 (13 pages), 2016. Keyword(s): Acoustics, Direct numerical simulations, Flow modeling and control, Input-output analysis, Jet noise. [bibtex-entry]



9. 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]



10. J. W. Nichols and M. R. Jovanovic. Input-output analysis of high-speed jet noise. In Proceedings of the 2014 Summer Program, Center for Turbulence Research, Stanford University/NASA, pages 251-260, 2014. Keyword(s): Acoustics, Flow modeling and control, Input-output analysis, Jet noise. [bibtex-entry]



11. M. R. Jovanovic, P. J. Schmid, and J. W. Nichols. Low-rank and sparse dynamic mode decomposition. In Center for Turbulence Research Annual Research Briefs, pages 139-152, 2012. Keyword(s): Dynamic Mode Decomposition, Flow modeling and control, Convex optimization, Sparsity. [bibtex-entry]



12. T. Sayadi, J. W. Nichols, P. J. Schmid, and M. R. Jovanovic. Dynamic mode decomposition of H-type transition to turbulence. In Proceedings of the 2012 Summer Program, Center for Turbulence Research, Stanford University/NASA, pages 5-14, 2012. Keyword(s): Boundary layers, Dynamic mode decomposition, Flow modeling and control, Navier-Stokes equations, Transition to turbulence. [bibtex-entry]

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