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3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall
Weber, A. and Schreiber, H. A. and Fuchs, R. and Steinert, W. (2002) 3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall. ASME Journal of Turbomachinery, Vo. 124, July 2002, pp. 358-366.
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| Document Type: | Article | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Additional Information: | LIDO-Berichtsjahr=2005, | ||||||||||
| Title: | 3-D Transonic Flow in a Compressor Cascade With Shock-Induced Corner Stall | ||||||||||
| Authors: |
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| Date: | 2002 | ||||||||||
| Journal or Publication Title: | ASME Journal of Turbomachinery | ||||||||||
| Refereed publication: | Yes | ||||||||||
| In ISI Web of Science: | Yes | ||||||||||
| Volume: | Vo. 124, July 2002 | ||||||||||
| Page Range: | pp. 358-366 | ||||||||||
| Status: | Published | ||||||||||
| Keywords: | Transonic compressor flow, 3-D test case | ||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||
| HGF - Program: | Aeronautics | ||||||||||
| HGF - Program Themes: | L - no assignement | ||||||||||
| DLR - Research area: | Aeronautics | ||||||||||
| DLR - Program: | L TT - Triebwerkstechnologien | ||||||||||
| DLR - Research theme (Project): | L - Fan and Compressor Technologies | ||||||||||
| Location: | Köln-Porz | ||||||||||
| Institutes and Institutions: | Institute of Propulsion Technology | ||||||||||
| Deposited By: | Herr Heinz-Adolf Schreiber | ||||||||||
| Deposited On: | 16 Sep 2005 | ||||||||||
| Last Modified: | 06 Jan 2010 13:36 |
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