Unit Reynolds number, Mach number and pressure gradient effects on laminar–turbulent transition in two-dimensional boundary layers-Reference-Cited by-同舟云学术

Unit Reynolds number, Mach number and pressure gradient effects on laminar–turbulent transition in two-dimensional boundary layers

Published:2018-05 Issue:5 Volume:59 Page:
ISSN:0723-4864
Container-title:Experiments in Fluids
language:en
Short-container-title:Exp Fluids

Author:

Risius Steffen^ORCID,Costantini Marco,Koch Stefan,Hein Stefan,Klein Christian

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Link

http://link.springer.com/article/10.1007/s00348-018-2538-8/fulltext.html

Reference71 articles.

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2. Arnal D (1992) Boundary layer transition: prediction, application to drag reduction. Tech. Rep. AGARD Rept, p 786

3. Arnal D, Vermeersch O (2011) Compressibility effects on laminar-turbulent boundary layer transition. Int J Eng Syst Model Simul 3(1–2):26–35. https://doi.org/10.1504/IJESMS.2011.038747

4. Arnal D, Casalis G, Cousteix J, Reneaux J (1997) Laminar-turbulent transition in subsonic boundary layers-research and applications in France. In: 28th fluid dynamics conference, American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1997-1905

5. Arnal D, Délery J (2004) Laminar–turbulent transition and shock wave/boundary layer interaction. In: RTO AVT lecture series on critical technologies for hypersonic vehicle development, RTO-EN-AVT-116, Rhode-St-Genèse, Belgium, pp 4-1–4-46

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