Kiock, R. (1994) Pressure Distribution on an isolated TPS 441 nacelle. Proceedings, AGARD Fluid Dynamics Panel.
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The demand for even more economic jet engines requires extensive experimental investigations of the complete flow field around wing-body-pylon (WBEP) configurations. The engine can be simulated best by pressure-driven devices, so-called Turbine-Powered Simulators (TPS). Though they have been applied for about 20 years, very few nacelle surface pressure measurements were carried out up to now. The reason is seen in the small size of the engine and in the poor theoretical capabilities in the past. Nowadays, WBEP configurations are handled by the Euler code, but experimental investigation of the isolated nacelle which is presented here.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=1994, pages=9,|
|Title:||Pressure Distribution on an isolated TPS 441 nacelle|
|Keywords:||Turbine-Powered Simulator, nacelle surface pressure measurements, axi symmetric nacelle of 5" fan diameter, base for validation of CFD code|
|Event Title:||Proceedings, AGARD Fluid Dynamics Panel|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||other|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||L ST - Starrflüglertechnologien|
|DLR - Research theme (Project):||L - Concepts & Integration|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||03 Apr 2006|
|Last Modified:||27 Apr 2009 10:05|
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