Numerical investigation of the inclined leading edge diffuser vane effects on the flow unsteadiness and noise characteristics in a transonic centrifugal compressor

A. Zamiri; B.J. Lee; J.T. Chung

doi:10.1115/GT2017-65117

Numerical investigation of the inclined leading edge diffuser vane effects on the flow unsteadiness and noise characteristics in a transonic centrifugal compressor

A. Zamiri
, B.J. Lee
, J.T. Chung

School of Civil, Aerospace and Design Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference Contribution (Conference Proceeding)

1 Citation (Scopus)

Original language	English
Title of host publication	Proceedings of the ASME Turbo Expo
DOIs	https://doi.org/10.1115/GT2017-65117
Publication status	Published - 2017

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@inproceedings{1b98c495746c44108ed5b3711560bb2e,

title = "Numerical investigation of the inclined leading edge diffuser vane effects on the flow unsteadiness and noise characteristics in a transonic centrifugal compressor",

author = "A. Zamiri and B.J. Lee and J.T. Chung",

year = "2017",

doi = "10.1115/GT2017-65117",

language = "English",

booktitle = "Proceedings of the ASME Turbo Expo",

}

TY - GEN

T1 - Numerical investigation of the inclined leading edge diffuser vane effects on the flow unsteadiness and noise characteristics in a transonic centrifugal compressor

AU - Zamiri, A.

AU - Lee, B.J.

AU - Chung, J.T.

PY - 2017

Y1 - 2017

UR - https://www.scopus.com/pages/publications/85028975203

U2 - 10.1115/GT2017-65117

DO - 10.1115/GT2017-65117

M3 - Conference Contribution (Conference Proceeding)

BT - Proceedings of the ASME Turbo Expo

ER -

Numerical investigation of the inclined leading edge diffuser vane effects on the flow unsteadiness and noise characteristics in a transonic centrifugal compressor

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