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A Closely Coupled Experimental and Numerical Approach for Hypersonic and High Enthalpy Flow Investigations Utilising the HEG Shock Tunnel and the DLR TAU Code - Part 1

Hannemann, Klaus and Martinez Schramm, Jan and Wagner, Alexander and Karl, Sebastian and Hannemann, Volker (2010) A Closely Coupled Experimental and Numerical Approach for Hypersonic and High Enthalpy Flow Investigations Utilising the HEG Shock Tunnel and the DLR TAU Code - Part 1. In: NATO Research and Technology Organisation. Aerothermodynamic Design, Review on Ground Testing andCFD, 29 March - 1 April 2010, Rhode St. Genese, Belgium. ISBN 978-92-837-0121-7

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Item URL in elib:https://elib.dlr.de/66184/
Document Type:Conference or Workshop Item (Lecture)
Title:A Closely Coupled Experimental and Numerical Approach for Hypersonic and High Enthalpy Flow Investigations Utilising the HEG Shock Tunnel and the DLR TAU Code - Part 1
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Martinez Schramm, Janjan.martinez (at) dlr.deUNSPECIFIED
Wagner, Alexanderalexander.wagner (at) dlr.deUNSPECIFIED
Karl, Sebastiansebastian.karl (at) dlr.deUNSPECIFIED
Hannemann, Volkervolker.hannemann (at) dlr.deUNSPECIFIED
Date:March 2010
Journal or Publication Title:NATO Research and Technology Organisation
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
ISBN:978-92-837-0121-7
Status:Published
Keywords:Hypersonic; Transition; SW/BL Interaction; Chemistry; TPS Materials; Ground Testing; Flight Extrapolation
Event Title:Aerothermodynamic Design, Review on Ground Testing andCFD
Event Location:Rhode St. Genese, Belgium
Event Type:Workshop
Event Dates:29 March - 1 April 2010
Organizer:von Karman Institute
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W - no assignment
DLR - Research area:Space
DLR - Program:W - no assignment
DLR - Research theme (Project):W - no assignment (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Wagner, Alexander
Deposited On:18 Apr 2011 13:18
Last Modified:18 Apr 2011 13:18

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