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Publications of N. Hildebrand
Journal articles
  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]


Conference articles
  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. Note: To appear. 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, 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]


  3. 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]


  4. 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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