Input-output analysis of complex hypersonic boundary layers
Author:
Affiliation:
1. University of Minnesota, Twin Cities
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1383
Reference14 articles.
1. Prehistory of Instability in a Hypersonic Boundary Layer
2. Transition and Stability of High-Speed Boundary Layers
3. Understanding effects of nose-cone bluntness on hypersonic boundary layer transition using input-output analysis
4. Sensitivity of hypersonic flows to distributed surface roughness using input-output analysis
5. Instabilities in Mach 6 Flow over a Cone with a Swept Fin
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2. A High-Order Finite-Difference Method for Linear Stability Analysis and Bi-orthogonal Decomposition of Hypersonic Boundary Layer Flow;AIAA SCITECH 2023 Forum;2023-01-19
3. Input/output analysis of a Mach-6 cooled-wall hypersonic boundary layer using the One-Way Navier-Stokes (OWNS) Equations;AIAA AVIATION 2022 Forum;2022-06-20
4. Assessment of Linear Methods for Analysis of Boundary Layer Instabilities on a Finned Cone at Mach 6;AIAA AVIATION 2022 Forum;2022-06-20
5. Sensitivity of Reacting Hypersonic Boundary Layers to n-periodic Surface Roughness;IUTAM Laminar-Turbulent Transition;2021-07-31
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