FILM COOLING IN A PLANE TURBINE CASCADE.

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

Research output: Chapter in Book/Report/Conference proceedingConference 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 languageEnglish (US)
Title of host publicationUnknown Host Publication Title
PublisherHemisphere Publ Corp
Pages37-43
Number of pages7
ISBN (Print)089116572X
StatePublished - Jan 1 1987

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    Goldstein, R. J., Eckert, E. R. G., & Ito, S. (1987). FILM COOLING IN A PLANE TURBINE CASCADE. In Unknown Host Publication Title (pp. 37-43). Hemisphere Publ Corp.