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Numerical Validation of a Free-Flying Scramjet Powered Vehicle at Realistic Wind Tunnel Conditions

Langener, Tobias and Steelant, Johan and Karl, Sebastian and Hannemann, Klaus (2014) Numerical Validation of a Free-Flying Scramjet Powered Vehicle at Realistic Wind Tunnel Conditions. Space Propulsion 2014, 19. - 22. Mai 2014, Cologne, Germany.

Full text not available from this repository.

Official URL: http://www.propulsion2014.com

Abstract

One of the major objectives of the EC-co funded research project LAPCAT II is demonstrating positive aero-propulsive balance of a scramjet propelled vehicle in a wind tunnel and comparing this data to numerical simulations for validation of the CFD tools. For this, the LAPCAT MR2 hypersonic cruiser was scaled to wind tunnel dimensions. An optimization of the internal flow path was necessary, to cope with the different flight conditions and constraints in the wind tunnel environment. Therefore, a study featuring reactive CFD simulations was carried out. It was found that the best way to achieve a high combustion efficiency is to use a staged injection scheme in the combustor. Furthermore, from the experimental campaign carried out in the high-enthalpy facility at DLR (High Enthalpy Shock Tunnel Göttingen, HEG) validation data is available to compare the numerical studies against. It was found that still some uncertainties in the prediction of the aero-propulsive balance exists, but the thrust level could be sufficiently predicted by the CFD simulations within the measurement accuracy.

Item URL in elib:https://elib.dlr.de/89141/
Document Type:Conference or Workshop Item (Speech)
Additional Information:Paper-Nr. SP2014-2971766, Session 23
Title:Numerical Validation of a Free-Flying Scramjet Powered Vehicle at Realistic Wind Tunnel Conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Langener, TobiasESA-ESTEC, NoordwijkUNSPECIFIED
Steelant, JohanJohan.Steelant (at) esa.intUNSPECIFIED
Karl, Sebastiansebastian.karl (at) dlr.deUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Date:2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-11
Series Name:Confereance Proceedings on CD-ROM
Status:Published
Keywords:computational fluid dynamics, airbreathing propulsion, hydrogen combustion
Event Title:Space Propulsion 2014
Event Location:Cologne, Germany
Event Type:international Conference
Event Dates:19. - 22. Mai 2014
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 - Numerische Verfahren und Simulation
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Micknaus, Ilka
Deposited On:28 Aug 2014 10:03
Last Modified:20 Mar 2015 16:10

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