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Bluntness Effects in Hypersonic Flow over Slender Cones and Wedges

Karl, Sebastian and Hannemann, Klaus and Hornung, Hans G. (2012) Bluntness Effects in Hypersonic Flow over Slender Cones and Wedges. In: 28th International Symposium on Shock Waves. Vol.2. Springer , Berlin, pp. 691-696. ISBN 978-3-642-25684-4. https://resolver.caltech.edu/CaltechAUTHORS:20200520-134452744

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Abstract

In hypersonic flow over slender bodies an important concern is the influence of nose bluntness on the viscous boundary layer behavior. This is particularly important in the consideration of boundary layer instability and transition. There exist numerous treatments, both theoretical and experimental on this subject. Representative excellent examples are [1] and [2] In this study we use the deviation from sharp–body theory of the heat flux distribution as obtained from computations of viscous perfect–gas flow over blunted slender bodies at zero incidence to estimate the point where the body has forgotten that it is blunt.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
https://doi.org/10.1007/978-3-642-25685-1_105DOIArticle
https://rdcu.be/b4iKXPublisherFree ReadCube access
ORCID:
AuthorORCID
Hornung, Hans G.0000-0002-4903-8419
Additional Information:© 2012 Springer-Verlag Berlin Heidelberg.
Group:GALCIT
Subject Keywords:Hypersonic Flow; Nose Radius; Slender Body; Boundary Layer Transition; Stanton Number
Record Number:CaltechAUTHORS:20200520-134452744
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20200520-134452744
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:103362
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:20 May 2020 21:01
Last Modified:20 May 2020 21:01

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