Passive Turbulence Generating Grid Arrangements in a Turbine Cascade Wind Tunnel

Abstract

Turbine cascade wind tunnels simulate Reynolds number and turbulence for the examination of flow phenomena such as boundary layer separation on the trailing portion of low pressure turbine blades. Axial chord-based Reynolds numbers considered in this study were 50k and 100k. Various passive, square-bar turbulence generating grid arrangements were explored to simulate turbulence in a turbine cascade test-section inlet, including two grid orientations: perpendicular to the inlet flow and parallel to the turbine cascade. A novel T-Bar turbulence grid configuration oriented parallel to the cascade was shown to produce better test section inlet flowfield uniformity than that produced by a perpendicular mesh grid. Improved periodicity in blade-to-blade surface pressure coefficient profiles was also observed with the parallel T-Bar grid.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Apr 02, 2014
Accession Number
AD1015089

Entities

People

  • Connor J. Wiese
  • Giovanni Allevato
  • Kurt P. Rouser
  • Michael J. Mcclearn
  • Richard Iii T. Guttman

Organizations

  • United States Air Force Academy

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Coefficients
  • Computational Fluid Dynamics
  • Dynamic Pressure
  • Flow
  • Fluid Flow
  • Free Stream
  • Layers
  • Measurement
  • Pressure Transducers
  • Reynolds Number
  • Static Pressure
  • Three Dimensional
  • Turbine Blades
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Mechanics and Fluid Dynamics.