Arnold, Richard and Suslov, Dmitry and Haidn, Oskar (2009) Influence Parameters on Film Cooling Effectiveness in a High Pressure Subscale Combustion Chamber. 47th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, FL, USA.
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In typical high performance rocket engines like the European Vulcain 2 or the Space Shuttle Main Engine (SSME) a significant reduction of thermal and structural loads is achieved by the application of film cooling with an acceptable loss in overall engine performance. Within the presented paper, the effectiveness of film cooling has been studied in a LOX/GH2 subscale rocket combustion chamber. Aiming at high performance first stage applications, combustion chamber pressures have been varied up to 12 MPa. Using GH2 with ambient temperatures for film cooling, typical influence parameters on film cooling effectiveness like film blowing rate, velocity ratio between film injection velocity and hot gas velocity, and film injection slot height have been investigated systematically at the European Research and Technology Test Facility P8.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Influence Parameters on Film Cooling Effectiveness in a High Pressure Subscale Combustion Chamber|
|Date:||5 January 2009|
|In ISI Web of Science:||No|
|Keywords:||Film cooling, rocket engine, high pressure|
|Event Title:||47th AIAA Aerospace Sciences Meeting|
|Event Location:||Orlando, FL, USA|
|Event Type:||international Conference|
|Event Dates:||2009-01-05 - 2009-01-08|
|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 - Schubkammertechnologie und Hochdruckverbrennung (old)|
|Institutes and Institutions:||Institute of Space Propulsion|
|Deposited By:||Richard Arnold|
|Deposited On:||13 Jan 2009|
|Last Modified:||27 Apr 2009 15:43|
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