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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

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 - 1987

UN SDGs

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

  1. SDG 7 - Affordable and Clean Energy
    SDG 7 Affordable and Clean Energy

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