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High Speed Intakes Thermal Research

Gruhn, Patrick and Gülhan, Ali (2011) High Speed Intakes Thermal Research. VKI/RTO Lecture Series AVT-195: Engine Intake Aerothermal Design: Subsonic to High Speed Application, 14.-16. Nov. 2011, Waterloo, Belgien.

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Abstract

Hypersonic intakes are subject to severe heat loads that have to be well understood in order to properly design a safe and reliable propulsion system. Therefore, thermal loads on the intake as well as high temperature effects that might influence the heat fluxes have to be studied beforehand, either analytically, numerically or experimentally. The objective of this lecture is to give an insight on such effects and thermal loads based on the experience gained in ground testing facilities.

Item URL in elib:https://elib.dlr.de/71755/
Document Type:Conference or Workshop Item (Lecture, Paper)
Title:High Speed Intakes Thermal Research
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gruhn, PatrickUNSPECIFIEDUNSPECIFIED
Gülhan, AliUNSPECIFIEDUNSPECIFIED
Date:9 November 2011
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hypersonic Intake, Scramjet
Event Title:VKI/RTO Lecture Series AVT-195: Engine Intake Aerothermal Design: Subsonic to High Speed Application
Event Location:Waterloo, Belgien
Event Type:Other
Event Dates:14.-16. Nov. 2011
Organizer:von Karman Institute for Fluid Dynamics (VKI)
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: Gruhn, Patrick
Deposited On:18 Nov 2011 12:59
Last Modified:18 Nov 2011 12:59

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