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October 1, 1996Journal of Turbomachinery

Film Cooling With Compound Angle Holes: Heat Transfer

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Authors

BSBasav SenDSDonald L. SchmidtDow Chemical (India)DBDavid G. BogardWalker (United States)

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Cite This Study

Sen et al. (1996) studied this question.

synapsesocial.com/papers/6a7d2e37166e996abdd5a5afhttps://doi.org/10.1115/1.2840937
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Also Consider

Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context:

  1. 1Film Cooling With Compound Angle Holes: Adiabatic Effectiveness1996 · 291 citations
  2. 2Experimental Investigation of Film Cooling With Ejection From a Row of Holes for the Application to Gas Turbine Blades1975 · 92 citations
  3. 3Analysis of Film Cooling and Full-Coverage Film Cooling of Gas Turbine Blades1984 · 73 citations
  4. 4The Influence of a Laminar Boundary Layer and Laminar Injection on Film Cooling Performance1982 · 37 citations
  5. 5Heat Transfer, Adiabatic Effectiveness, and Injectant Distributions Downstream of a Single Row and Two Staggered Rows of Compound Angle Film-Cooling Holes1992 · 62 citations