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Influence of Heat Capacity Ratio on the Interaction between the External Flow and Nozzle Flow of a Scramjet

Hirschen, Christian and Gruhn, Patrick and Gülhan, Ali (2006) Influence of Heat Capacity Ratio on the Interaction between the External Flow and Nozzle Flow of a Scramjet. In: 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference (AIAA-2006-8095). 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference, 2006-11-06 - 2006-11-09, Canberra (Australien).

Full text not available from this repository.

Abstract

As part of a graduate college financed by the German National Research Council (DFG), an experimental study on nozzle flows was carried out at the German aerospace center (DLR). The tests were performed at a free-stream Mach number Ma∞ = 7 in the H2K wind tunnel of the wind tunnel department in Cologne. The Reynolds number was varied in order to simulate the influence of different flight altitudes of a scramjet vehicle. The effects of different heat capacity ratios have been investigated by using gases with higher and lower heat capacity ratios than air. The obtained experimental results are discussed and compared with CFD calculations. Furthermore, an analysis on the effect of a Reynolds number and Mach number variation was carried out with a complete scramjet model. In both cases pressure measurements and Schlieren photographs were used in order investigate the flow properties.

Item URL in elib:https://elib.dlr.de/47796/
Document Type:Conference or Workshop Item (Speech)
Title:Influence of Heat Capacity Ratio on the Interaction between the External Flow and Nozzle Flow of a Scramjet
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hirschen, ChristianUniversität StuttgartUNSPECIFIEDUNSPECIFIED
Gruhn, PatrickUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Gülhan, AliUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2006
Journal or Publication Title:14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
American Institute of Aeronautics and Astronautics, UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Status:Published
Keywords:keine
Event Title:14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference
Event Location:Canberra (Australien)
Event Type:international Conference
Event Start Date:6 November 2006
Event End Date:9 November 2006
Organizer:American Institute of Aeronautics and Astronautics
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 - Antriebsystemtechnik - Antriebskonzepte (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By:INVALID USER
Deposited On:28 Mar 2007
Last Modified:24 Apr 2024 19:09

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