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Effect of Circumferential Grooves on the Aerodynamic Performance of an Axial Single-Stage Transonic Compressor

Müller, Martin W. and Schiffer, Heinz-Peter and Hah, Chunill (2007):
Effect of Circumferential Grooves on the Aerodynamic Performance of an Axial Single-Stage Transonic Compressor.
In: Volume 6: Turbo Expo 2007, Parts A and B, DOI: 10.1115/GT2007-27365,
[Online-Edition: https://doi.org/10.1115/GT2007-27365],
[Conference or Workshop Item]

Item Type: Conference or Workshop Item
Erschienen: 2007
Creators: Müller, Martin W. and Schiffer, Heinz-Peter and Hah, Chunill
Title: Effect of Circumferential Grooves on the Aerodynamic Performance of an Axial Single-Stage Transonic Compressor
Language: English
Title of Book: Volume 6: Turbo Expo 2007, Parts A and B
Divisions: 16 Department of Mechanical Engineering > Institute of Gas Turbines and Aerospace Propulsion (GLR)
16 Department of Mechanical Engineering
Date Deposited: 04 Apr 2018 20:36
DOI: 10.1115/GT2007-27365
Official URL: https://doi.org/10.1115/GT2007-27365
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