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Hypersonic Boundary-Layer Transition in the DLR High Enthalpy Shock Tunnel Göttingen (HEG) – Part 1

Wartemann, Viola and Wagner, Alexander (2015) Hypersonic Boundary-Layer Transition in the DLR High Enthalpy Shock Tunnel Göttingen (HEG) – Part 1. Seminar of Sandia National Laboratories, 23. March 2015, Albuquerque, USA.

Full text not available from this repository.

Abstract

Preceding studies in the High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) and corresponding numerical studies using the NOLOT stability code revealed that carbon fibre reinforced carbon ceramic (C/C) surfaces can be utilized to damp hypersonic boundary layer instabilities leading to a delay of boundary layer transition onset. The given talk provided an overview on the conducted studies and future plans.

Item URL in elib:https://elib.dlr.de/95881/
Document Type:Conference or Workshop Item (Speech)
Title:Hypersonic Boundary-Layer Transition in the DLR High Enthalpy Shock Tunnel Göttingen (HEG) – Part 1
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wartemann, Violaviola.wartemann (at) dlr.deUNSPECIFIED
Wagner, Alexanderalexander.wagner (at) dlr.deUNSPECIFIED
Date:23 March 2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hypersonic Boundary-Layer Transition, HEG, ultrasonically absorptive coating, C/C, NOLOT
Event Title:Seminar of Sandia National Laboratories
Event Location:Albuquerque, USA
Event Type:Other
Event Dates:23. March 2015
Organizer:Sandia National Laboratories
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 - Shefex III
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Wartemann, Viola
Deposited On:20 Apr 2015 12:01
Last Modified:20 Apr 2015 12:01

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