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Shock Shape Transition on Spherically Blunted Conesin Hypersonic Flows

Martinez Schramm, Jan and Hannemann, Klaus and Hornung, Hans G. (2017) Shock Shape Transition on Spherically Blunted Conesin Hypersonic Flows. 31st International Symposium on Shock Waves (ISSW31), 09.-14. Juli 2017, Nagoya, Japan.

Full text not available from this repository.

Official URL: http://akagi.nuae.nagoya-u.ac.jp/issw31/

Abstract

Spherically blunted cones are commonly utilized as re-entry or entry capsules. Depending on the cone angle, the shock shape is either dominated by the spherical nose or the conical part. In flight a transition between these two situations might occur and this can result in undesirable effects on the aerodynamic stability. To understand the shock shape transition behaviour in more detail, a systematic numerical and experimental study is ongoing. In the present article, the influence of vibrational non-equilibrium compared to frozen flow is discussed for sphere-cone configurations at zero degree angle of attack.

Item URL in elib:https://elib.dlr.de/111873/
Document Type:Conference or Workshop Item (Speech)
Title:Shock Shape Transition on Spherically Blunted Conesin Hypersonic Flows
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Martinez Schramm, Janjan.martinez (at) dlr.deUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Hornung, Hans G.california institute of technology, pasadena, caUNSPECIFIED
Date:2017
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:blunted cone, sonic line, shock tunnel, computational fluid dynamics, high temperature effects
Event Title:31st International Symposium on Shock Waves (ISSW31)
Event Location:Nagoya, Japan
Event Type:international Conference
Event Dates:09.-14. Juli 2017
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 - Anlagen u. Messtechnik
Location: Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Bachmann, Barbara
Deposited On:12 Jan 2018 14:01
Last Modified:12 Jan 2018 14:01

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