Hochschulschrift
Experimental investigations of the casing boundary layer of a two stage low speed axial compressor
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Dimensions
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21 cm
- Extent
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[VIII], 128 S.
- Language
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Englisch
- Notes
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Ill., graph. Darst.
Hannover, Univ., Diss., 1999
- Keyword
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Mehrstufiger Axialverdichter
Dreidimensionale Strömung
Strömungsfeld
Gehäuse
Grenzschichtströmung
- Creator
- Table of contents
- Rights
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Last update
-
11.06.2025, 1:45 PM CEST
Data provider
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Object type
- Hochschulschrift
Associated
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Investigation of Multiharmonic Effects in a Single Stage High Speed Compressor
A Holistic Approach for the Generic Preliminary Design of Axial Compressor and Turbine Annulus Contours
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Influence of Different Gases on the Design Point of an Industrial Axial Compressor and Deduced Aerodynamical Rematching Methodology
Acoustic resonance in a high-speed axial compressor
3D Profile Design and Optimization of a Rotor for a Low Speed Axial Compressor Wind Tunnel
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades
Influence of labyrinth seals in cavities on the flow of an axial compressor
Influence of labyrinth seals in cavities on the flow of an axial compressor
Experimental investigation of unsteady flow phenomena in a three-stage axial compressor
Effect of clocking on unsteady rotor blade loading in a low-speed axial compressor at design and off-design operating conditions
Investigation of Multiharmonic Effects in a Single Stage High Speed Compressor
A Holistic Approach for the Generic Preliminary Design of Axial Compressor and Turbine Annulus Contours
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