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Bluntness Effects in Hypersonic FLow over Slender Cones and Wedges

Karl, Sebastian and Hannemann, Klaus and Hans G., Hornung (2012) Bluntness Effects in Hypersonic FLow over Slender Cones and Wedges. In: 28th International Symposium on Shock Waves Shock Waves 2, Vol. 2. Springer Verlag, Berlin Heidelberg. pp. 691-696. ISBN 978-3-642-25684-4.

Full text not available from this repository.

Official URL: http://link.springer.com/chapter/10.1007/978-3-642-25685-1_105

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. 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.

Document Type:Contribution to a Collection
Title:Bluntness Effects in Hypersonic FLow over Slender Cones and Wedges
Authors:
AuthorsInstitution or Email of Authors
Karl, SebastianUNSPECIFIED
Hannemann, KlausUNSPECIFIED
Hans G., HornungCaltech
Date:2012
Journal or Publication Title:28th International Symposium on Shock Waves
Refereed publication:Yes
In Open Access:Yes
In ISI Web of Science:No
Volume: Vol. 2
DOI:10.1007/978-3-642-25685-1_105
Page Range:pp. 691-696
Editors:
EditorsEmail
Kontis, KonstantinosUNSPECIFIED
Publisher:Springer Verlag, Berlin Heidelberg
Series Name:Shock Waves 2
ISBN:978-3-642-25684-4
Status:Published
Keywords:Hypersonic, transition, bluntness
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Sebastian Karl
Deposited On:20 Nov 2012 14:17
Last Modified:20 Nov 2012 14:17

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