Görtler Number Evaluation for Laminar Separated Hypersonic Compression Ramp Flow
Author:
Affiliation:
1. RWTH Aachen University, 52056 Aachen, Germany
Funder
RWTH Aachen University
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference17 articles.
1. GörtlerH. “Über eine Dreidimensionale Instabilität Laminarer Grenzschichten an Konkaven Wänden,” Ph.D. Thesis, Univ. of Göttingen, Göttingen, Germany, 1940.
2. Analysis of hypersonic shock-wave laminar boundary-layer interaction phenomena
3. Numerical simulation of Görtler vortices in hypersonic compression ramps
4. Stability of Hypersonic Boundary Layers over a Compression Corner
5. Görtler Vortices in Hypersonic Flow on Compression Ramps
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1. Görtler Instability and Transition in Compressible Flows;AIAA Journal;2023-12-29
2. Methods of experimental investigations of the Görtler instability in boundary layers (review);Thermophysics and Aeromechanics;2022-08-10
3. Theory-based prediction of separation angle and peak pressure for laminar separated hypersonic compression corner flows;Physics of Fluids;2021-08
4. Leading-edge bluntness effects on hypersonic three-dimensional flows over a compression ramp;Journal of Fluid Mechanics;2021-07-30
5. Unsteady effects in a hypersonic compression ramp flow with laminar separation;Journal of Fluid Mechanics;2021-02-04
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