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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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.
|Document Type:||Conference or Workshop Item (Lecture, Paper)|
|Title:||High Speed Intakes Thermal Research|
|Date:||9 November 2011|
|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 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 assignement|
|DLR - Research theme (Project):||L -- no assignement|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology|
|Deposited By:||Patrick Gruhn|
|Deposited On:||18 Nov 2011 12:59|
|Last Modified:||18 Nov 2011 12:59|
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