Numerical Study of Interference Effects on wing-mounted advanced Engine Concepts
Rossow, C.-C. (1994) Numerical Study of Interference Effects on wing-mounted advanced Engine Concepts. Proceedings 19th ICAS-Congress/AIAA Systems Conference 18.-23. September 1994, Anaheim, California, USA.
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The aerodynamic interference effects of three different wing-mounted engine concepts, namely a conventional turbofan, a very high bypass ratio turbofan, and an ultra high bypass ratio ducted propfan are investigated by the solution of the Euler equations. Due to the interference of fan jet and wing, the ultra high bypass engine shows the largest interference. A variation of position reveals for both the very high and the ultra high bypass ratio engine a potential for a close coupling of engine and airframe.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=1994, pages=11,|
|Title:||Numerical Study of Interference Effects on wing-mounted advanced Engine Concepts|
|Keywords:||Interference Effects, wing-mounted engine concepts, conventional turbofan, very high bypass ratio turbofan, ultra high bypass ratio ducted propfan|
|Event Title:||Proceedings 19th ICAS-Congress/AIAA Systems Conference 18.-23. September 1994, Anaheim, California, USA|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L - no assignement|
|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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