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Post Flight Experiments of the SHEFEX I Configuration in the High Enthalpy Shock Tunnel Göttingen (HEG)

Martinez Schramm, Jan and Wagner, Alexander and Wolfram, Jeremy and Hannemann, Klaus and Barth, Tarik and Mulot, Jean-Daniel (2009) Post Flight Experiments of the SHEFEX I Configuration in the High Enthalpy Shock Tunnel Göttingen (HEG). 27th International Symposium on Shock Waves, 19.-24. Juli 2009, St. Petersburg. (Unpublished)

Full text not available from this repository.

Official URL: http://www.ioffe.ru/ISSW27/

Abstract

One important aspect of the SHarp Edge Flight EXperiment (SHEFEX) program of the German Aerospace Center (DLR) is the post flight analysis of the data gathered during the flight of SHEFEX-I. One part of the analysis is the experimental simulation of a flight point at an altitude of approximately 20 km in the High Enthalpy Shock Tunnel Göttingen (HEG). To conduct these experiments a very complex wind tunnel model of the SHEFEX-I configuration has been designed, machined and instrumented by DLR. The experimental campaign performed in HEG included the measurement of surface pressure and surface heat fluxes on the wind tunnel model. Additionally flow visualisation with the Schlieren- and Shadowgraph method has been applied and flow velocity measured by the use of Particle Image Velocimetry (PIV) have been accomplished. As a supplementation to the heat flux measurements with thermocouples, the technique of IR-thermography of the model surface has been tested for the first time in HEG to gain access to the complete flow topology on the surface of the wind tunnel model. To achieve a adequate experimental database an exceptional large number of runs has been performed in HEG and supplementary each experiment has been numerically conducted by applying the DLR Tau code to model the flow in HEG. The comparison between the numerical and experimental data for surface pressure and surface heat flux is the main focus in this paper. The comparison between the wind tunnel results and the data gathered during flight will be discussed conclusively.

Item URL in elib:https://elib.dlr.de/60872/
Document Type:Conference or Workshop Item (Paper)
Title:Post Flight Experiments of the SHEFEX I Configuration in the High Enthalpy Shock Tunnel Göttingen (HEG)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Martinez Schramm, JanJan.Martinez (at) dlr.deUNSPECIFIED
Wagner, AlexanderAlexander.Wagner (at) dlr.deUNSPECIFIED
Wolfram, JeremyJeremy.Wolfram (at) dlr.deUNSPECIFIED
Hannemann, KlausKlaus.Hannemann (at) dlr.deUNSPECIFIED
Barth, TarikTarik.Bart (at) dlr.deUNSPECIFIED
Mulot, Jean-DanielUNSPECIFIEDUNSPECIFIED
Date:July 2009
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:SHEFEX I HEG flight experiment shock tunnel
Event Title:27th International Symposium on Shock Waves
Event Location:St. Petersburg
Event Type:international Conference
Event Dates:19.-24. Juli 2009
Organizer:27th International Symposium on Shock Waves
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Raumfahrzeugsysteme - Anlagen u. Messtechnik (old), W - SHEFEX Programm (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Martinez Schramm, Jan
Deposited On:17 Nov 2009 13:18
Last Modified:01 Dec 2018 19:46

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