Hochschulschrift
Influence of labyrinth seals in cavities on the flow of an axial compressor
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Dimensions
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21 cm
- Extent
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xxiv, 159 Seiten
- Language
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Englisch
- Notes
-
Illustrationen
Gottfried Wilhelm Leibniz Universität Hannover, Dissertation, 2017
- Bibliographic citation
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Berichte aus dem Institut für Turbomaschinen und Fluid-Dynamik / Gottfried Wilhelm Leibniz Universität Hannover ; Band 13 (2018)
- Classification
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Ingenieurwissenschaften und Maschinenbau
- Event
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Veröffentlichung
- (where)
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Hannover
- (who)
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Institut für Turbomaschinen und Fluid-Dynamik
- (when)
-
2018
- Creator
- Table of contents
- Rights
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Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Last update
-
11.03.2025, 12:08 PM CET
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.
Object type
- Hochschulschrift
Associated
- Flores Galindo, Diego Rodrigo
- Institut für Turbomaschinen und Fluid-Dynamik
Time of origin
- 2018
Other Objects (12)
Influence of labyrinth seals in cavities on the flow of an axial compressor
Acoustic resonance in a high-speed axial compressor
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Unsteady Flow in a Labyrinth Seal
Experimental investigation of unsteady flow phenomena in a three-stage axial compressor
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades
Coupling stability-enhancing mechanism with compact self-recirculating injection in an axial flow compressor
Beam dynamics of the FRANZ bunch compressor using realistic fields with a focus on the rebuncher cavities
A Holistic Approach for the Generic Preliminary Design of Axial Compressor and Turbine Annulus Contours
Experimental investigations of the casing boundary layer of a two stage low speed axial compressor
The Aero-Thermal Impact of Rim Seal Purge Flow in Axial Turbines
Influence of honeycomb structures on straight-through labyrinth seal aerodynamics
Influence of labyrinth seals in cavities on the flow of an axial compressor
Acoustic resonance in a high-speed axial compressor
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Unsteady Flow in a Labyrinth Seal
Experimental investigation of unsteady flow phenomena in a three-stage axial compressor
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades
Coupling stability-enhancing mechanism with compact self-recirculating injection in an axial flow compressor
Beam dynamics of the FRANZ bunch compressor using realistic fields with a focus on the rebuncher cavities
A Holistic Approach for the Generic Preliminary Design of Axial Compressor and Turbine Annulus Contours
Experimental investigations of the casing boundary layer of a two stage low speed axial compressor
The Aero-Thermal Impact of Rim Seal Purge Flow in Axial Turbines
Influence of honeycomb structures on straight-through labyrinth seal aerodynamics
Influence of labyrinth seals in cavities on the flow of an axial compressor
Acoustic resonance in a high-speed axial compressor
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Unsteady Flow in a Labyrinth Seal
Experimental investigation of unsteady flow phenomena in a three-stage axial compressor
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades
Coupling stability-enhancing mechanism with compact self-recirculating injection in an axial flow compressor
Beam dynamics of the FRANZ bunch compressor using realistic fields with a focus on the rebuncher cavities
A Holistic Approach for the Generic Preliminary Design of Axial Compressor and Turbine Annulus Contours
Experimental investigations of the casing boundary layer of a two stage low speed axial compressor
The Aero-Thermal Impact of Rim Seal Purge Flow in Axial Turbines