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 - Jan 1 1987

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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",

month = jan,

day = "1",

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publisher = "Hemisphere Publ Corp",

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T1 - FILM COOLING IN A PLANE TURBINE CASCADE.

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AU - Eckert, E. R G

AU - Ito, S.

PY - 1987/1/1

Y1 - 1987/1/1

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.

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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

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