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Ground Testing Synthesis of the LAPCAT II Small Scale Flight Experiment Configuration Scramjet Flow Path

Martinez Schramm, Jan and Hannemann, Klaus and Karl, Sebastian and Defoort, Sebastien and Viguier, Paul and Steelant, Johan (2015) Ground Testing Synthesis of the LAPCAT II Small Scale Flight Experiment Configuration Scramjet Flow Path. American Institute of Aeronautics and Astronautics. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 06. - 09. July 2015, Glasgow, Scotland, United Kingdom. DOI: 10.2514/6.2015-3627

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/abs/10.2514/6.2015-3627

Abstract

This paper reports on the experiments on a a scramjet powered flight experiment configuration. The 1.5 m long wind tunnel model consists of intake, combustor and thrust nozzle and is designed for a flight Mach number of 7.4. The outer mold line of this small scale flight configuration (SSFE) was derived from the full scale Mach 8 cruiser MR 2 proposed by ESA-ESTEC within the EC co-funded LAPCAT II project. In the framework of LAPCAT II, the two major European free jet facilities, namely the High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) and the F4 hot shot facility of the French Aerospace Lab (ONERA) were used to perform these measurements. The core tests in HEG and F4 is emphasizing the Mach 7.4-8 flight conditions. The paper gives an experimental synthesis on both campaigns and discusses the complementary results in both facilities.

Item URL in elib:https://elib.dlr.de/98403/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA 2015-3627
Title:Ground Testing Synthesis of the LAPCAT II Small Scale Flight Experiment Configuration Scramjet Flow Path
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Martinez Schramm, Janjan.martinez (at) dlr.deUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Karl, Sebastiansebastian.karl (at) dlr.deUNSPECIFIED
Defoort, SebastienONERAUNSPECIFIED
Viguier, PaulONERAUNSPECIFIED
Steelant, JohanESA-ESTEC, NLUNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2015-3627
Page Range:pp. 1-12
Publisher:American Institute of Aeronautics and Astronautics
Series Name:Conference Proceedings online
Status:Published
Keywords:small scale flight configuration (SSFE), LAPCAT II, supersonic combustion, HEG
Event Title:20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Event Location:Glasgow, Scotland, United Kingdom
Event Type:international Conference
Event Dates:06. - 09. July 2015
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 - Anlagen u. Messtechnik
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Micknaus, Ilka
Deposited On:29 Oct 2015 09:35
Last Modified:29 Oct 2015 09:35

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