- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
Axial transonic compressor performance enhancement with circumferential grooves ; volume:11 ; number:1 ; year:2020 ; pages:153-161
Mechanical sciences ; 11, Heft 1 (2020), 153-161
- Creator
-
Ahmad, Naseem
Zheng, Qun
Fawzy, Hamza
Yaqoob, Tasneem
Abdu Ahmad, Salman
Bin, Jiang
- DOI
-
10.5194/ms-11-153-2020
- URN
-
urn:nbn:de:101:1-2020051405173707596938
- Rights
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
14.08.2025, 10:51 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
- Ahmad, Naseem
- Zheng, Qun
- Fawzy, Hamza
- Yaqoob, Tasneem
- Abdu Ahmad, Salman
- Bin, Jiang
Other Objects (12)
Simplified Design Theory for highly loaded axial compressor rotors and experimental study of two transonic examples
Circumferential groove casing treatments in centrifugal compressor aerodynamics
Eliminating the head instability of an axial-flow pump using axial grooves
Performance Evaluation of Transonic Axial Flow Compressor under Distorted Conditions by Groove Casing Technique with Tip Injection and Surface Roughness Effects
A Casing Treatment with Axial Grooves for Centrifugal Compressors
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
Influence of blade geometry on secondary flow development in a transonic centrifugal compressor
Influence of Blade Geometry on Secondary Flow Development in a Transonic Centrifugal Compressor
The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
Evaporation modeling of water droplets in a transonic compressor cascade under fogging conditions
Acoustic resonance in a high-speed axial compressor
Grooves
Simplified Design Theory for highly loaded axial compressor rotors and experimental study of two transonic examples
Circumferential groove casing treatments in centrifugal compressor aerodynamics
Eliminating the head instability of an axial-flow pump using axial grooves
Performance Evaluation of Transonic Axial Flow Compressor under Distorted Conditions by Groove Casing Technique with Tip Injection and Surface Roughness Effects
A Casing Treatment with Axial Grooves for Centrifugal Compressors
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
Influence of blade geometry on secondary flow development in a transonic centrifugal compressor
Influence of Blade Geometry on Secondary Flow Development in a Transonic Centrifugal Compressor
The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
Evaporation modeling of water droplets in a transonic compressor cascade under fogging conditions
Acoustic resonance in a high-speed axial compressor
Grooves
Simplified Design Theory for highly loaded axial compressor rotors and experimental study of two transonic examples
Circumferential groove casing treatments in centrifugal compressor aerodynamics
Eliminating the head instability of an axial-flow pump using axial grooves
Performance Evaluation of Transonic Axial Flow Compressor under Distorted Conditions by Groove Casing Technique with Tip Injection and Surface Roughness Effects
A Casing Treatment with Axial Grooves for Centrifugal Compressors
The transonic compressor with non-uniform tip clearance : effects on aerodynamics and aeroelasticity
Influence of blade geometry on secondary flow development in a transonic centrifugal compressor
Influence of Blade Geometry on Secondary Flow Development in a Transonic Centrifugal Compressor
The transonic compressor with non-uniform tip clearance: Effects on aerodynamics and aeroelasticity
Evaporation modeling of water droplets in a transonic compressor cascade under fogging conditions
Acoustic resonance in a high-speed axial compressor