OPTIMUM SLOT SIZE AND LOCATION IN A RADIAL VANE IMPELLER FOR BETTER CENTRIFUGAL PUMP PERFORMANCE
Last updated: 04 Jan 2025
10.21608/asat.2001.24768
Flow Pattern, Vortex, Turbomachinery, Impeller, Computational Fluid Dynamics, Centrifugal Pump
M.
Hussien
S.E.
Egyptian Armed Forces.
A.
Lotfy
H.
Egyptian Armed Forces.
H.
Abdalla
M.
Egyptian Armed Forces.
I.
Saleh
Egyptian Armed Forces.
9
ASAT Conference, 8-10 May 2001
4547
2001-05-01
2019-01-15
2001-05-01
1
17
2090-0678
2636-364X
https://asat.journals.ekb.eg/article_24768.html
https://asat.journals.ekb.eg/service?article_code=24768
11
Original Article
737
Journal
International Conference on Aerospace Sciences and Aviation Technology
https://asat.journals.ekb.eg/
OPTIMUM SLOT SIZE AND LOCATION IN A RADIAL VANE IMPELLER FOR BETTER CENTRIFUGAL PUMP PERFORMANCE
Details
Type
Article
Created At
22 Jan 2023