Impeller treatment for a centrifugal fan using splitter vanes - A CFD approach

Research output: Chapter in Book/Report/Conference proceedingConference contribution

3 Citations (Scopus)

Abstract

In a centrifugal impeller the flow field is highly complex with flow reversal taking place on the suction side of impeller. Generally the performance of a centrifugal fan could be enhanced by introducing splitter vanes at judiciously selected locations. An extensive numerical whole field analysis on the effect of splitter vanes placed in discreet regions of suspected separation points is possible using CFD. This paper examines the effect of splitter vanes corresponding to various geometrical locations on the impeller. It is found that splitter vanes located at the impeller leading edge improves the static pressure recovery of the fan. However, splitters provided near to the trailing edge of the impeller adversely affect the static pressure recovery of the fan.

Original languageEnglish
Title of host publicationProceedings of the World Congress on Engineering 2011, WCE 2011
Pages1981-1986
Number of pages6
Volume3
Publication statusPublished - 14-11-2011
EventWorld Congress on Engineering 2011, WCE 2011 - London, United Kingdom
Duration: 06-07-201108-07-2011

Conference

ConferenceWorld Congress on Engineering 2011, WCE 2011
CountryUnited Kingdom
CityLondon
Period06-07-1108-07-11

Fingerprint

Fans
Computational fluid dynamics
Recovery
Suction
Reversal
Flow Field
Flow fields
Fan

All Science Journal Classification (ASJC) codes

  • Computer Science(all)
  • Engineering(all)
  • Applied Mathematics

Cite this

Madhwesh, N., Karanth, K. V., & Sharma, N. Y. (2011). Impeller treatment for a centrifugal fan using splitter vanes - A CFD approach. In Proceedings of the World Congress on Engineering 2011, WCE 2011 (Vol. 3, pp. 1981-1986)
Madhwesh, N. ; Karanth, K. Vasudeva ; Sharma, N. Yagnesh. / Impeller treatment for a centrifugal fan using splitter vanes - A CFD approach. Proceedings of the World Congress on Engineering 2011, WCE 2011. Vol. 3 2011. pp. 1981-1986
@inproceedings{2e8ba87e1726428a8bd6b65b2bd9cf40,
title = "Impeller treatment for a centrifugal fan using splitter vanes - A CFD approach",
abstract = "In a centrifugal impeller the flow field is highly complex with flow reversal taking place on the suction side of impeller. Generally the performance of a centrifugal fan could be enhanced by introducing splitter vanes at judiciously selected locations. An extensive numerical whole field analysis on the effect of splitter vanes placed in discreet regions of suspected separation points is possible using CFD. This paper examines the effect of splitter vanes corresponding to various geometrical locations on the impeller. It is found that splitter vanes located at the impeller leading edge improves the static pressure recovery of the fan. However, splitters provided near to the trailing edge of the impeller adversely affect the static pressure recovery of the fan.",
author = "N. Madhwesh and Karanth, {K. Vasudeva} and Sharma, {N. Yagnesh}",
year = "2011",
month = "11",
day = "14",
language = "English",
isbn = "9789881925152",
volume = "3",
pages = "1981--1986",
booktitle = "Proceedings of the World Congress on Engineering 2011, WCE 2011",

}

Madhwesh, N, Karanth, KV & Sharma, NY 2011, Impeller treatment for a centrifugal fan using splitter vanes - A CFD approach. in Proceedings of the World Congress on Engineering 2011, WCE 2011. vol. 3, pp. 1981-1986, World Congress on Engineering 2011, WCE 2011, London, United Kingdom, 06-07-11.

Impeller treatment for a centrifugal fan using splitter vanes - A CFD approach. / Madhwesh, N.; Karanth, K. Vasudeva; Sharma, N. Yagnesh.

Proceedings of the World Congress on Engineering 2011, WCE 2011. Vol. 3 2011. p. 1981-1986.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

TY - GEN

T1 - Impeller treatment for a centrifugal fan using splitter vanes - A CFD approach

AU - Madhwesh, N.

AU - Karanth, K. Vasudeva

AU - Sharma, N. Yagnesh

PY - 2011/11/14

Y1 - 2011/11/14

N2 - In a centrifugal impeller the flow field is highly complex with flow reversal taking place on the suction side of impeller. Generally the performance of a centrifugal fan could be enhanced by introducing splitter vanes at judiciously selected locations. An extensive numerical whole field analysis on the effect of splitter vanes placed in discreet regions of suspected separation points is possible using CFD. This paper examines the effect of splitter vanes corresponding to various geometrical locations on the impeller. It is found that splitter vanes located at the impeller leading edge improves the static pressure recovery of the fan. However, splitters provided near to the trailing edge of the impeller adversely affect the static pressure recovery of the fan.

AB - In a centrifugal impeller the flow field is highly complex with flow reversal taking place on the suction side of impeller. Generally the performance of a centrifugal fan could be enhanced by introducing splitter vanes at judiciously selected locations. An extensive numerical whole field analysis on the effect of splitter vanes placed in discreet regions of suspected separation points is possible using CFD. This paper examines the effect of splitter vanes corresponding to various geometrical locations on the impeller. It is found that splitter vanes located at the impeller leading edge improves the static pressure recovery of the fan. However, splitters provided near to the trailing edge of the impeller adversely affect the static pressure recovery of the fan.

UR - http://www.scopus.com/inward/record.url?scp=80755150081&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=80755150081&partnerID=8YFLogxK

M3 - Conference contribution

SN - 9789881925152

VL - 3

SP - 1981

EP - 1986

BT - Proceedings of the World Congress on Engineering 2011, WCE 2011

ER -

Madhwesh N, Karanth KV, Sharma NY. Impeller treatment for a centrifugal fan using splitter vanes - A CFD approach. In Proceedings of the World Congress on Engineering 2011, WCE 2011. Vol. 3. 2011. p. 1981-1986