Review: Active Control of Shock-associated Unsteady Flow Phenomena in Aeroengines - Suppression Techniques for Transonic Cascade Flutter and Supersonic Jet Noise -
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Classification
-
Ingenieurwissenschaften und Maschinenbau
- Event
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Veröffentlichung
- (where)
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Berlin
- (who)
-
Technische Universität Berlin
- (when)
-
2014
- Creator
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Watanabe, Toshinori
- DOI
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10.14279/depositonce-38
- Handle
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11303/195
- URN
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urn:nbn:de:101:1-201802277507
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
14.08.2025, 10:50 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Watanabe, Toshinori
- Technische Universität Berlin
Time of origin
- 2014
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Hysteresis in Supersonic Flow Past a Plane Cascade of Cylindrical Rods
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Evaporation modeling of water droplets in a transonic compressor cascade under fogging conditions
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Numerical investigation of unsteady transonic shock-boundary-layer interaction for aeronautical applications
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Steady and unsteady performance of a transonic compressor stage with non-axisymmetric end walls
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