A High-Order Finite-Difference Method for Linear Stability Analysis and Bi-orthogonal Decomposition of Hypersonic Boundary Layer Flow
Author:
Affiliation:
1. University of California Los Angeles
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1043
Reference47 articles.
1. Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers
2. BOUNDARY-LAYER RECEPTIVITY TO FREESTREAM DISTURBANCES
3. Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions
4. The continuous spectrum of the Orr-Sommerfeld equation. Part 2. Eigenfunction expansions
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1. A new very high-order finite-difference method for linear stability analysis and bi-orthogonal decomposition of hypersonic boundary layer flow;Journal of Computational Physics;2024-09
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