Effects of end-walls on flows in a highly loaded compressor cascade with double-circular-arc blades
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
In: Physics of Fluids 34 (5) : 055124 (2022-05-01)
- Event
-
Veröffentlichung
- (where)
-
Hamburg
- (who)
-
Universitätsbibliothek der Technischen Universität Hamburg
- (when)
-
2022
- Creator
- DOI
-
10.15480/882.4915
- URN
-
urn:nbn:de:gbv:830-882.0187488
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:42 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.
Associated
- Jin, Yan
- Li, Changyong
- Du, Juan
- Zhang, Hongwu
- Universitätsbibliothek der Technischen Universität Hamburg
Time of origin
- 2022
Other Objects (12)
Prediction of compressor blade erosion experiments in a cascade based on flat plate specimen
Aerodynamic optimisation of highly loaded turbine cascade blades for heavy duty gas turbine applications
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Recent progress in turbine blade and compressor blisk regeneration
Surface roughness of real operationally used compressor blade and blisk
Potential of additively manufactured particle damped compressor blades: A literature review
Tools and Strategies for Grinding of Riblets on Freeformed Compressor Blades
Effects of Rotation on the Flow Structure in a Compressor Cascade
Numerical Assessment of Virtual Control Surfaces for Load Alleviation on Compressor Blades
An automated multi-objective optimization approach for aerodynamic 3D compressor blade design
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades
A theoritical investigation of the jet-flap compressor cascade in incompressible flow
Prediction of compressor blade erosion experiments in a cascade based on flat plate specimen
Aerodynamic optimisation of highly loaded turbine cascade blades for heavy duty gas turbine applications
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Recent progress in turbine blade and compressor blisk regeneration
Surface roughness of real operationally used compressor blade and blisk
Potential of additively manufactured particle damped compressor blades: A literature review
Tools and Strategies for Grinding of Riblets on Freeformed Compressor Blades
Effects of Rotation on the Flow Structure in a Compressor Cascade
Numerical Assessment of Virtual Control Surfaces for Load Alleviation on Compressor Blades
An automated multi-objective optimization approach for aerodynamic 3D compressor blade design
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades
A theoritical investigation of the jet-flap compressor cascade in incompressible flow
Prediction of compressor blade erosion experiments in a cascade based on flat plate specimen
Aerodynamic optimisation of highly loaded turbine cascade blades for heavy duty gas turbine applications
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Recent progress in turbine blade and compressor blisk regeneration
Surface roughness of real operationally used compressor blade and blisk
Potential of additively manufactured particle damped compressor blades: A literature review
Tools and Strategies for Grinding of Riblets on Freeformed Compressor Blades
Effects of Rotation on the Flow Structure in a Compressor Cascade
Numerical Assessment of Virtual Control Surfaces for Load Alleviation on Compressor Blades
An automated multi-objective optimization approach for aerodynamic 3D compressor blade design
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades