Study of Impingement Heat Transfer with Rough Surfaces.

Abstract

The effects of surface roughness on impingement cooling of a gas turbine blade were determined experimentally. The study was conducted in a heated flow two-dimensional cascade tunnel. Results showed that roughening of the impingement surfaces decreased the cooling effectiveness from that of a smooth surface in an optimal cooling configuration. However, the roughened surfaces increased the cooling effectiveness over that of a smooth surface in a nonoptimal configuration. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1975
Accession Number
ADA022617

Entities

People

  • E. Mcfarland
  • Widen Tabakoff

Organizations

  • University of Cincinnati

Tags

DTIC Thesaurus Topics

  • Gas Turbine Blades
  • Gas Turbines
  • Heat Transfer
  • Rotor Blades (Turbomachinery)
  • Roughness
  • Surface Roughness
  • Turbine Blades
  • Turbines
  • Turbomachinery
  • Two Dimensional

Readers

  • Fluid Mechanics and Fluid Dynamics.