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Experimental Investigation of Supersonic Combustion in the HIEST and HEG Free Piston Driven Shock Tunnels

Martinez Schramm, Jan and Sunami, Tesuji and Itoh, Katsuhiro and Hannemann, Klaus (2010) Experimental Investigation of Supersonic Combustion in the HIEST and HEG Free Piston Driven Shock Tunnels. 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 25.-28. Juli 2010, Nashville, USA. ISBN 978-1-60086-747-7.

Full text not available from this repository.

Official URL: http://www.aiaa.org

Abstract

Ground based testing of a supersonic combustion ramjet (scramjet) configuration used in the framework of the HyShot IV flight were carried out in the High Enthalpy Shock Tunnel (HIEST) of the Japan Aerospace Exploration Agency (JAXA) Kakuda Space Center and the High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR). The objective of these investigations was to study the same hydrogen fuelled scramjet configuration in both large scale free piston driven shock tunnels and to compare the combustor performance. The full scale wind tunnel models consisted of an intake, a combustor and exhaust surfaces. The utilised test conditions aimed at duplicating Mach 7.5 flight conditions in the altitude range of 28 – 30 km. Gaseous hydrogen was injected into the combustion chamber by a wall mounted hypermixer injector developed by JAXA. The characteristics of the combustion process, in particular the change from steady supersonic combustion to a transient combustor flow, was investigated in both facilities by varying the fuel equivalence ratio. Time resolved surface pressure measurements in the combustor and on the exhaust surfaces as well as high speed flow visualisation was performed.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Experimental Investigation of Supersonic Combustion in the HIEST and HEG Free Piston Driven Shock Tunnels
Authors:
AuthorsInstitution or Email of Authors
Martinez Schramm, JanUNSPECIFIED
Sunami, TesujiJAXA, Japan
Itoh, KatsuhiroJAXA, Japan
Hannemann, KlausUNSPECIFIED
Date:2010
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-18
Series Name:AIAA meeting papers on Disc, DVD-Rom
ISBN:978-1-60086-747-7
Status:Published
Keywords:scramjet, high enthalpy, combustion, shock tunnel, DLR, JAXA
Event Title:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Event Location:Nashville, USA
Event Type:international Conference
Event Dates:25.-28. Juli 2010
Organizer:AIAA
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 - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Dagmar Brennecke-Hosseinzadeh
Deposited On:22 Sep 2010 09:13
Last Modified:22 Sep 2010 09:13

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