Analysis of the Effects of Wake Passage on Heat Transfer in a Linear Turbine Cascade

Abstract

This study investigated the effect of wake passage On the heat transfer in a linear turbine cascade. The apparatus used was the Air-Force Institute of Technology linear Turbine Cascade Test Facility (TCTF). The TCTF was fitted with a be Pulley system to facilitate a series of translating bars. The bars, when passed d upstream of the cascade, created a series of wakes. The parameters varied were freestream model Reynolds number and bar conditions, i.e. , bars in, bars out, and bar passing frequency. One blade in the TCTF was instrumented to allow pressure and temperature measurements at discrete points on the blade's surface. From the pressure and temperature data the convective heat transfer coefficient at these discrete locations was calculated. Results were compared to previous TCTF heat transfer data, empirical solutions, and other wake passage experiments. For all tests with closely spaced bars, the effect of wake passing on the heat transfer of the blade was similar to the effect of grid-generated 10% freestream turbulence on the cascade.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1993
Accession Number
ADA273729

Entities

People

  • Kevin S. Allen

Organizations

  • Air Force Test Center

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Equations Of State
  • Fluid Dynamics
  • Fluid Mechanics
  • Frequency
  • Gas Turbines
  • Heat Energy
  • Heat Transfer
  • Heat Transfer Coefficients
  • Measurement
  • Pressure Measurement
  • Pressure Transducers
  • Reynolds Number
  • Test Facilities
  • Turbines
  • Turbulence

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Mechanical Engineering/Mechanics of Materials.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster