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25678

EXPERIMENTAL AND THEORETICAL INVESTIGATION OF LOSSES IN A RADIAL COMPRESSOR STAGE

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Last updated: 04 Jan 2025

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Abstract

A model has been assumed to predict the hydraulic and disc friction losses in a radial compressor stage. A potential three dimensional flow field inside the impeller is solved, by using TSONICMR program. Then, the hydraulic and disc friction losses sere predicted for the impeller, vaneless diffuser and the collector. Experimental investigation has been carried out for a radial compressor stage, in order to verify the validity of the assumed model. The pressure ratio and efficiency were measured for different mass flow rats. at different rotating speeds. The results showed satisfactory agreement with that predicted .

DOI

10.21608/asat.1991.25678

Authors

First Name

K.

Last Name

Saad Eldin

MiddleName

M.

Affiliation

Senior Engineer of a Power workshop, Armed Forces.

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Orcid

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First Name

Ibrahim

Last Name

Saleh

MiddleName

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Affiliation

Assoc. Prof., Mech. Power Dept.

Email

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City

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Orcid

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First Name

Ali

Last Name

Elzahabi

MiddleName

-

Affiliation

Prof., Aircraft Dept.. Military Tech. College.

Email

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City

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Orcid

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First Name

Salah

Last Name

Elfeki

MiddleName

-

Affiliation

Head of Aircraft Group. Tech. Ins. Of Armed Forces. Egypt.

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Orcid

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Volume

4

Article Issue

ASAT CONFLENCE 14-16 May 1991 , CAIRO

Related Issue

4667

Issue Date

1991-05-01

Receive Date

2019-01-22

Publish Date

1991-05-01

Page Start

191

Page End

198

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_25678.html

Detail API

https://asat.journals.ekb.eg/service?article_code=25678

Order

17

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

EXPERIMENTAL AND THEORETICAL INVESTIGATION OF LOSSES IN A RADIAL COMPRESSOR STAGE

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Article

Created At

22 Jan 2023