Impact of Additive Manufacturing Surface Roughness on the Aerodynamic Performance of Axial Compressor Blades
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Extent
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1 Online-Ressource.
- Language
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Englisch
- Bibliographic citation
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Impact of Additive Manufacturing Surface Roughness on the Aerodynamic Performance of Axial Compressor Blades ; day:4 ; month:7 ; year:2024 ; pages:1-8
International journal of aeronautical and space sciences ; (4.7.2024), 1-8
- Creator
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Lim, Sukhyeon
Ko, Youngeon
Hong, Dunam
Kim, Myungho
Song, Seung Jin
- Contributor
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SpringerLink (Online service)
- DOI
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10.1007/s42405-024-00769-7
- URN
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urn:nbn:de:101:1-2409231258095.636803136802
- Rights
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Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
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15.08.2025, 7:30 AM CEST
Data provider
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Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Lim, Sukhyeon
- Ko, Youngeon
- Hong, Dunam
- Kim, Myungho
- Song, Seung Jin
- SpringerLink (Online service)
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Surface roughness of real operationally used compressor blade and blisk
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Axial compressor blades tip leakage flow control using natural aspiration
An automated multi-objective optimization approach for aerodynamic 3D compressor blade design
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades
Experimental Aerodynamic and Aeroelastic Investigation of a Transonic Compressor Rotor with Reduced Blade Count
Performance of a Low Speed Axial Compressor Rotor Blade Row under Different Inlet Distortions
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Combining shape-adaptive blades and active flow control in a multi-stage axial compressor: a numerical study
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Recent progress in turbine blade and compressor blisk regeneration
Aerodynamic validation for compressor blades’ structural morphing concepts
Surface roughness of real operationally used compressor blade and blisk
Influence of Blade Aspect Ratio on Axial Compressor Efficiency
Axial compressor blades tip leakage flow control using natural aspiration
An automated multi-objective optimization approach for aerodynamic 3D compressor blade design
Numerical Prediction of The Notch Effect of Riblets on Axial Compressor Blades
Experimental Aerodynamic and Aeroelastic Investigation of a Transonic Compressor Rotor with Reduced Blade Count
Performance of a Low Speed Axial Compressor Rotor Blade Row under Different Inlet Distortions
Low-inertia centrifugal compressor wheels: Aerodynamic and mechanical design
Combining shape-adaptive blades and active flow control in a multi-stage axial compressor: a numerical study
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