FILM COOLING IN A PLANE TURBINE CASCADE.

R. J. Goldstein; E. R G Eckert; S. Ito

FILM COOLING IN A PLANE TURBINE CASCADE.

R. J. Goldstein, E. R G Eckert, S. Ito

Mechanical Engineering

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

2 Scopus citations

Abstract

Results of a mass transfer study show the influence of surface curvature on film cooling effectiveness. Tests using simulated turbine blades are reported for injected gas to mainstream-air density ratios near unity and two, over a range of injection rates.

Original language	English (US)
Title of host publication	Unknown Host Publication Title
Publisher	Hemisphere Publ Corp
Pages	37-43
Number of pages	7
ISBN (Print)	089116572X
State	Published - 1987

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

Find It

Find It at U of M Libraries

Cite this

@inproceedings{1f10427a5e7c4255937de4b720856aba,

title = "FILM COOLING IN A PLANE TURBINE CASCADE.",

abstract = "Results of a mass transfer study show the influence of surface curvature on film cooling effectiveness. Tests using simulated turbine blades are reported for injected gas to mainstream-air density ratios near unity and two, over a range of injection rates.",

author = "Goldstein, \{R. J.\} and Eckert, \{E. R G\} and S. Ito",

year = "1987",

language = "English (US)",

isbn = "089116572X",

publisher = "Hemisphere Publ Corp",

pages = "37--43",

booktitle = "Unknown Host Publication Title",

}

TY - GEN

T1 - FILM COOLING IN A PLANE TURBINE CASCADE.

AU - Goldstein, R. J.

AU - Eckert, E. R G

AU - Ito, S.

PY - 1987

Y1 - 1987

N2 - Results of a mass transfer study show the influence of surface curvature on film cooling effectiveness. Tests using simulated turbine blades are reported for injected gas to mainstream-air density ratios near unity and two, over a range of injection rates.

AB - Results of a mass transfer study show the influence of surface curvature on film cooling effectiveness. Tests using simulated turbine blades are reported for injected gas to mainstream-air density ratios near unity and two, over a range of injection rates.

UR - https://www.scopus.com/pages/publications/0023089463

UR - https://www.scopus.com/inward/citedby.url?scp=0023089463&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:0023089463

SN - 089116572X

SP - 37

EP - 43

BT - Unknown Host Publication Title

PB - Hemisphere Publ Corp

ER -

FILM COOLING IN A PLANE TURBINE CASCADE.

Abstract

UN SDGs

Find It

Other files and links

Fingerprint

Cite this