Numerical simulation of fundamental breakdown of a laminar boundary-layer at Mach 4.5-Reference-Cited by-同舟云学术

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Numerical simulation of fundamental breakdown of a laminar boundary-layer at Mach 4.5

Published:1993-08-22 Issue: Volume: Page:
ISSN:
Container-title:5th International Aerospace Planes and Hypersonics Technologies Conference
language:
Short-container-title:

Author:

Adams N.¹,Kleiser L.¹

Affiliation:

1. DLR, Goettingen, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-5027

Reference26 articles.

1. I. Adauns, N.A., 1993 Nuinerisclie Siinulation von Transitionstnechmismen in kotnprcssiblcn Grenzschichtcn, DLR-FB 93-29 (also doctoral thesis, Technischc Univcrsitiit Miinchen) (in Gerinm).

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1. Prandtl number effects on the hydrodynamic stability of compressible boundary layers: flow–thermodynamics interactions;Journal of Fluid Mechanics;2022-09-07

2. Multi-scale study of the transitional shock-wave boundary layer interaction in hypersonic flow;Theoretical and Computational Fluid Dynamics;2021-11-29

3. Transition scenario in hypersonic axisymmetrical compression ramp flow;Journal of Fluid Mechanics;2020-11-17

4. Subharmonic transition to turbulence in a flat-plate boundary layer at Mach number 4.5;Journal of Fluid Mechanics;1996-06-25

5. Comparison of temporal and spatial direct numerical simulation of compressible boundary-layer transition;AIAA Journal;1996-04

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