Pressures on a Slender, Axisymmetric Body at High Angle of Attack in a Very Low Turbulence Level Air Stream.

Abstract

The report describes the work and results of the past year on this contract to investigate the pressures on slender bodies at high incidence. Results are presented from two models used to investigate the transient nature of the pressures and from one model with two interchangeable noses used only for determining time-averaged pressures. The results show a dependence on roll angle but indicate that a regular and universal state may exist for the flow, and any other states are perturbations between the two possible hands of the regular state. Local side force and normal force distributions are presented which show that both are affected by the vortex flow field. The investigations have largely been performed in a low speed, very low turbulence wind tunnel. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1979
Accession Number
ADA080472

Entities

People

  • B. L. Hunt
  • P. C. Dexter

Organizations

  • University of Bristol

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Computer Programs
  • Flow
  • Flow Fields
  • Flow Visualization
  • Geometry
  • High Angles
  • Measurement
  • Nose Tips
  • Orientation (Direction)
  • Pressure Distribution
  • Pressure Measurement
  • Pressure Transducers
  • Reynolds Number
  • Slender Bodies
  • Test Facilities
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computational Fluid Dynamics (CFD)
  • Theoretical Analysis.