Heat/mass transfer measurement on the tip surface of rotor blade with squlear rim

Jun Su Park; Dong Hyun Lee; Woo Jin Lee; Hyung Hee Cho; Dong Ho Rhee; Shin Hyung Kang

doi:10.1063/1.3464948

Heat/mass transfer measurement on the tip surface of rotor blade with squlear rim

Jun Su Park, Dong Hyun Lee, Woo Jin Lee, Hyung Hee Cho, Dong Ho Rhee, Shin Hyung Kang

Department of Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

1 Citation (Scopus)

Abstract

The present study investigates local heat/mass transfer characteristics on blade tip surface with squealer rim. A linear cascade experimental setup consists of three large scale airfoils was used. The axial chord length and turning angle of test blade are 237 mm and 126°, respectively. Heat/mass transfer coefficients were measured with three different rim heights (3%, 6% and 9% of axial chord length) and fixed tip clearance (2% of axial chord length). Main flow Reynolds number based on axial chord length is 1.5×105. Naphthalene sublimation method is used to measure the detailed mass transfer coefficient on the blade tip surface. The heat/mass transfer results show that as the rim height increases, the peak values on the upstream region of the tip surface decreases and moves to the suction side rim. At the downstream region of the tip surface, the pitch-wise averaged heat/mass transfer coefficients increases as the rim height increases.

Original language	English
Title of host publication	10th Asian International Conference on Fluid Machinery, AICFM
Pages	952-958
Number of pages	7
DOIs	https://doi.org/10.1063/1.3464948
Publication status	Published - 2010
Event	10th Asian International Conference on Fluid Machinery, AICFM - Kuala Lumpur, Malaysia Duration: 2010 Oct 21 → 2010 Oct 23

Publication series

Name	AIP Conference Proceedings
Volume	1225
ISSN (Print)	0094-243X
ISSN (Electronic)	1551-7616

Other

Other	10th Asian International Conference on Fluid Machinery, AICFM
Country/Territory	Malaysia
City	Kuala Lumpur
Period	10/10/21 → 10/10/23

Bibliographical note

Funding Information:
Funding:NIH(NIGMS)https://www.nih.gov/(grant

All Science Journal Classification (ASJC) codes

Physics and Astronomy(all)

Access to Document

10.1063/1.3464948

Cite this

@inproceedings{122fa7899dbc453c874b4dfe981b4718,

title = "Heat/mass transfer measurement on the tip surface of rotor blade with squlear rim",

abstract = "The present study investigates local heat/mass transfer characteristics on blade tip surface with squealer rim. A linear cascade experimental setup consists of three large scale airfoils was used. The axial chord length and turning angle of test blade are 237 mm and 126°, respectively. Heat/mass transfer coefficients were measured with three different rim heights (3%, 6% and 9% of axial chord length) and fixed tip clearance (2% of axial chord length). Main flow Reynolds number based on axial chord length is 1.5×105. Naphthalene sublimation method is used to measure the detailed mass transfer coefficient on the blade tip surface. The heat/mass transfer results show that as the rim height increases, the peak values on the upstream region of the tip surface decreases and moves to the suction side rim. At the downstream region of the tip surface, the pitch-wise averaged heat/mass transfer coefficients increases as the rim height increases.",

author = "Park, {Jun Su} and Lee, {Dong Hyun} and Lee, {Woo Jin} and Cho, {Hyung Hee} and Rhee, {Dong Ho} and Kang, {Shin Hyung}",

note = "Funding Information: Funding:NIH(NIGMS)https://www.nih.gov/(grant; 10th Asian International Conference on Fluid Machinery, AICFM ; Conference date: 21-10-2010 Through 23-10-2010",

year = "2010",

doi = "10.1063/1.3464948",

language = "English",

isbn = "9780735407695",

series = "AIP Conference Proceedings",

pages = "952--958",

booktitle = "10th Asian International Conference on Fluid Machinery, AICFM",

}

Park, JS, Lee, DH, Lee, WJ, Cho, HH, Rhee, DH & Kang, SH 2010, Heat/mass transfer measurement on the tip surface of rotor blade with squlear rim. in 10th Asian International Conference on Fluid Machinery, AICFM. AIP Conference Proceedings, vol. 1225, pp. 952-958, 10th Asian International Conference on Fluid Machinery, AICFM, Kuala Lumpur, Malaysia, 10/10/21. https://doi.org/10.1063/1.3464948

TY - GEN

T1 - Heat/mass transfer measurement on the tip surface of rotor blade with squlear rim

AU - Park, Jun Su

AU - Lee, Dong Hyun

AU - Lee, Woo Jin

AU - Cho, Hyung Hee

AU - Rhee, Dong Ho

AU - Kang, Shin Hyung

N1 - Funding Information: Funding:NIH(NIGMS)https://www.nih.gov/(grant

PY - 2010

Y1 - 2010

N2 - The present study investigates local heat/mass transfer characteristics on blade tip surface with squealer rim. A linear cascade experimental setup consists of three large scale airfoils was used. The axial chord length and turning angle of test blade are 237 mm and 126°, respectively. Heat/mass transfer coefficients were measured with three different rim heights (3%, 6% and 9% of axial chord length) and fixed tip clearance (2% of axial chord length). Main flow Reynolds number based on axial chord length is 1.5×105. Naphthalene sublimation method is used to measure the detailed mass transfer coefficient on the blade tip surface. The heat/mass transfer results show that as the rim height increases, the peak values on the upstream region of the tip surface decreases and moves to the suction side rim. At the downstream region of the tip surface, the pitch-wise averaged heat/mass transfer coefficients increases as the rim height increases.

AB - The present study investigates local heat/mass transfer characteristics on blade tip surface with squealer rim. A linear cascade experimental setup consists of three large scale airfoils was used. The axial chord length and turning angle of test blade are 237 mm and 126°, respectively. Heat/mass transfer coefficients were measured with three different rim heights (3%, 6% and 9% of axial chord length) and fixed tip clearance (2% of axial chord length). Main flow Reynolds number based on axial chord length is 1.5×105. Naphthalene sublimation method is used to measure the detailed mass transfer coefficient on the blade tip surface. The heat/mass transfer results show that as the rim height increases, the peak values on the upstream region of the tip surface decreases and moves to the suction side rim. At the downstream region of the tip surface, the pitch-wise averaged heat/mass transfer coefficients increases as the rim height increases.

UR - http://www.scopus.com/inward/record.url?scp=78549258133&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=78549258133&partnerID=8YFLogxK

U2 - 10.1063/1.3464948

DO - 10.1063/1.3464948

M3 - Conference contribution

AN - SCOPUS:78549258133

SN - 9780735407695

T3 - AIP Conference Proceedings

SP - 952

EP - 958

BT - 10th Asian International Conference on Fluid Machinery, AICFM

T2 - 10th Asian International Conference on Fluid Machinery, AICFM

Y2 - 21 October 2010 through 23 October 2010

ER -

Heat/mass transfer measurement on the tip surface of rotor blade with squlear rim

Abstract

Publication series

Other

Bibliographical note

All Science Journal Classification (ASJC) codes

Access to Document

Other files and links

Fingerprint

Cite this