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Numerical Investigation on Transition of Shock Induced Boundary Layer

Tanaki, Kohsuke and Inaba, Kazuaki and Yamamoto, Makoto (2009) Numerical Investigation on Transition of Shock Induced Boundary Layer. In: 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics , Reston, VA, Art. No. 2009-1529. ISBN 978-1-60086-973-0. https://resolver.caltech.edu/CaltechAUTHORS:20200117-085601492

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Abstract

The purpose or this paper is to examine the application or empirical models or boundary layer transition to the situation of shock wave propagation. Two-dimensional numerical simulations of shock wave propagation and shock-induced boundary layer motion were performed with the turbulent intermittency transport model of Menter et al (2004). The Launder-Sharma low-Reynolds k-ϵ model was used for the turbulence model and the boundary layer profiles were compared against the theoretical laminar profiles and the empirical turbulent profiles. The predicted transition Reynolds number in the present study was in good agreement with the shock tube experimental data.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
https://doi.org/10.2514/6.2009-1529DOIArticle
Additional Information:© 2009 by the American Institute of Aeronautics and Astronautics, Inc. Published online: 15 Jun 2012.
Group:GALCIT
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AIAA Paper2009-1529
Record Number:CaltechAUTHORS:20200117-085601492
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20200117-085601492
Official Citation:Numerical Investigation on Transition of Shock Induced Boundary Layer. Kohsuke Tanaki, Kazuaki Inaba, and Makoto Yamamoto. 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. January 2009; doi: 10.2514/6.2009-1529
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:100782
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:17 Jan 2020 17:08
Last Modified:17 Jan 2020 17:13

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