Simultaneous Flow Visualization and Unsteady Lift Measurement on an Oscillating Lifting Surface,

Abstract

Boundary layer and trailing edge flow activities were recorded using hydrogen bubble flow visualization techniques on an oscillating lifting surface in a two-dimensional water tunnel. Simultaneous with flow documentation, unsteady lift was measured over a range of reduced frequencies from 0.5 to 10. Unsteady loads using classical, inviscid theories were predicted for the experimental conditions investigated. Reduced frequency bands exhibiting poor agreement between experiment and theory were identified and a correlation to observed flow phenomena was accomplished. The results support the use of a separate viscous model near the trailing edge coupled with an inviscid flow field model to predict unsteady loads. The results further show that for certain reduced frequency bands, classical inviscid solutions may be applicable and adequate.

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1984
Accession Number
ADP004157

Entities

People

  • J. E. Johnson
  • J. F. Unruh
  • R. L. Bass

Organizations

  • Southwest Research Institute

Tags

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Flow
  • Flow Fields
  • Flow Visualization
  • Frequency
  • Frequency Bands
  • Inviscid Flow
  • Lifting Surfaces
  • Measurement
  • Trailing Edges
  • Two Dimensional
  • United States
  • United States Air Force Academy
  • Water Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.