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Direct Numerical Simulation of Subharmonic Transition in a Flat-Plate Boundary-Layer at Mach 4.5
Adams, N.A. (1992) Direct Numerical Simulation of Subharmonic Transition in a Flat-Plate Boundary-Layer at Mach 4.5. Seminarvortrag, QMW London, 16.12.1992.
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| Document Type: | Conference or Workshop Item (Speech) | ||||
|---|---|---|---|---|---|
| Additional Information: | LIDO-Berichtsjahr=1992, | ||||
| Title: | Direct Numerical Simulation of Subharmonic Transition in a Flat-Plate Boundary-Layer at Mach 4.5 | ||||
| Authors: |
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| Date: | 1992 | ||||
| Status: | Published | ||||
| Keywords: | Direct Numerical Simulation, Flat-Plate Boundary-Layer, Transition, Compressible Boundary Layer | ||||
| Event Title: | Seminarvortrag, QMW London, 16.12.1992 | ||||
| HGF - Research field: | UNSPECIFIED | ||||
| HGF - Program: | Aeronautics | ||||
| HGF - Program Themes: | L - no assignement | ||||
| DLR - Research area: | UNSPECIFIED | ||||
| DLR - Program: | L TG - Querschnittstechnologien | ||||
| DLR - Research theme (Project): | UNSPECIFIED | ||||
| Location: | Köln-Porz , Braunschweig , Göttingen | ||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Theoretische Strömungsmechanik | ||||
| Deposited By: | elib DLR-Beauftragter | ||||
| Deposited On: | 03 Apr 2006 | ||||
| Last Modified: | 27 Apr 2009 10:35 |
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