Boundary Layer Transition on the LEA Hypersonic Vehicle Forebody-Reference-Cited by-同舟云学术

Boundary Layer Transition on the LEA Hypersonic Vehicle Forebody

Published:2012-09-24 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference
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Author:

Fedioun I.¹,Orlik E.¹

Affiliation:

1. ICARE-CNRS

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5864

Reference33 articles.

1. Transient growth: A factor in bypass transition

2. Modal Linear Stability of the Near-Wall Flow on a Hypersonic Forebody

3. 5Ferrier, M. "Etudedelastabilitéetprévisiondelatransitionlaminaire/turbulent del'écoulement procheparoi surl'avantcorps d'un véhicule hypersonique," PhD thesis fromUniversitéd'Orléans,2008. Available online at http://tel.archives-ouvertes.fr/docs/00/35/02/63/PDF/Memoire_Ferrier.pdf

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