Hochschulschrift
Aerodynamic Losses in an Aero Engine Centrifugal Compressor with a Close-Coupled Pipe-Diffuser and a Radial-Axial Deswirler
- Alternative title
-
Aerodynamische Verluste in einem Triebwerksradialverdichter mit eng gekoppeltem Pipe Diffusor und radial-axiale Umlenkbeschaufelung
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
In: München : Hut, 2015 (Strömungsmechanik)
RWTH Aachen University, Dissertation, 2015
- Classification
-
Ingenieurwissenschaften und Maschinenbau
- Event
-
Veröffentlichung
- (where)
-
Aachen
- (who)
-
Universitätsbibliothek der RWTH Aachen
- (when)
-
2015
- Creator
- Contributor
- URN
-
urn:nbn:de:hbz:82-rwth-2015-017297
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:47 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
- Wilkosz, Benjamin Eduard
- Jeschke, Peter
- Olivier, Herbert
- Universitätsbibliothek der RWTH Aachen
Time of origin
- 2015
Other Objects (12)
Low-inertia centrifugal compressor wheels: Aerodynamic and mechanical design
Experimental investigation on the diffuser flow of a centrifugal compressor stage with pipe diffuser
Circumferential groove casing treatments in centrifugal compressor aerodynamics
Flow structure and stability of a turbocharger centrifugal compressor
Acoustic resonance in a high-speed axial compressor
Numerical analysis of a centrifugal compressor operating with supercritical CO2
Aerodynamic optimization of low-pressure axial fans
Coupled vibration of unshrouded centrifugal compressor impellers. Part I: Experimental investigation
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Process integration and automated multi-objective optimization supporting aerodynamic compressor design
A Casing Treatment with Axial Grooves for Centrifugal Compressors
1968 – 2021 Centrifugal Compressor Research : Research projects of the past ten years
Low-inertia centrifugal compressor wheels: Aerodynamic and mechanical design
Experimental investigation on the diffuser flow of a centrifugal compressor stage with pipe diffuser
Circumferential groove casing treatments in centrifugal compressor aerodynamics
Flow structure and stability of a turbocharger centrifugal compressor
Acoustic resonance in a high-speed axial compressor
Numerical analysis of a centrifugal compressor operating with supercritical CO2
Aerodynamic optimization of low-pressure axial fans
Coupled vibration of unshrouded centrifugal compressor impellers. Part I: Experimental investigation
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Process integration and automated multi-objective optimization supporting aerodynamic compressor design
A Casing Treatment with Axial Grooves for Centrifugal Compressors
1968 – 2021 Centrifugal Compressor Research : Research projects of the past ten years
Low-inertia centrifugal compressor wheels: Aerodynamic and mechanical design
Experimental investigation on the diffuser flow of a centrifugal compressor stage with pipe diffuser
Circumferential groove casing treatments in centrifugal compressor aerodynamics
Flow structure and stability of a turbocharger centrifugal compressor
Acoustic resonance in a high-speed axial compressor
Numerical analysis of a centrifugal compressor operating with supercritical CO2
Aerodynamic optimization of low-pressure axial fans
Coupled vibration of unshrouded centrifugal compressor impellers. Part I: Experimental investigation
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Process integration and automated multi-objective optimization supporting aerodynamic compressor design
A Casing Treatment with Axial Grooves for Centrifugal Compressors