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Baumert, W. and Hoheisel, H. and Kiock, R. and Rossow, C. C. and Ronzheimer, A. and Capdevila, H. (1990) Aspects of Theoretical and Experimental Investigations on Airframe/Engine Integration Problems. In: Proc. 17th Congress of The ICAS. 17th Congress of the ICAS, 9-14 September 1990, Stockholm, Sweden.
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Abstract
The study describes the flow field around an Airbus-type configuration with a conventional turbofan engine. The three-dimensional Euler equations were solved using a cell-vertex method using a multi-block structure. A half model with a turbo-powered simulator was investigatedat low speed. Results show good agreement between theory and experiment.
| Item URL in elib: | https://elib.dlr.de/24242/ | |||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Paper) | |||||||||||||||||||||
| Additional Information: | LIDO-Berichtsjahr=1990, | |||||||||||||||||||||
| Title: | Aspects of Theoretical and Experimental Investigations on Airframe/Engine Integration Problems | |||||||||||||||||||||
| Authors: |
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| Date: | 1990 | |||||||||||||||||||||
| Journal or Publication Title: | Proc. 17th Congress of The ICAS | |||||||||||||||||||||
| Open Access: | No | |||||||||||||||||||||
| Gold Open Access: | No | |||||||||||||||||||||
| In SCOPUS: | No | |||||||||||||||||||||
| In ISI Web of Science: | No | |||||||||||||||||||||
| Status: | Published | |||||||||||||||||||||
| Keywords: | Aircraft Engine | |||||||||||||||||||||
| Event Title: | 17th Congress of the ICAS, 9-14 September 1990, Stockholm, Sweden | |||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport (old) | |||||||||||||||||||||
| HGF - Program: | other | |||||||||||||||||||||
| HGF - Program Themes: | other | |||||||||||||||||||||
| DLR - Research area: | Aeronautics | |||||||||||||||||||||
| DLR - Program: | no assignment | |||||||||||||||||||||
| DLR - Research theme (Project): | UNSPECIFIED | |||||||||||||||||||||
| Location: | Köln-Porz | |||||||||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology | |||||||||||||||||||||
| Deposited By: | DLR-Beauftragter, elib | |||||||||||||||||||||
| Deposited On: | 02 Apr 2006 | |||||||||||||||||||||
| Last Modified: | 27 Apr 2009 05:22 |
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