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3D Transonic Flow in a Compressor Cascade with Shock-Induced Corner Stall
Schreiber, H.A. and Weber, A. and Fuchs, R. and Steinert, W. (2001) 3D Transonic Flow in a Compressor Cascade with Shock-Induced Corner Stall. The 46th ASME International Gas Turbine & Aeroengine Technical Congress, New Orleans, USA, June 4-7, 2001.
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| Document Type: | Conference or Workshop Item (Paper) | ||||||||||
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| Additional Information: | LIDO-Berichtsjahr=2001, | ||||||||||
| Title: | 3D Transonic Flow in a Compressor Cascade with Shock-Induced Corner Stall | ||||||||||
| Authors: |
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| Date: | 2001 | ||||||||||
| Status: | Published | ||||||||||
| Event Title: | The 46th ASME International Gas Turbine & Aeroengine Technical Congress, New Orleans, USA, June 4-7, 2001 | ||||||||||
| Organizer: | ASME | ||||||||||
| 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: | elib DLR-Beauftragter | ||||||||||
| Deposited On: | 16 Sep 2005 | ||||||||||
| Last Modified: | 06 Jan 2010 13:18 |
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