Transonic Interactions of Unsteady Vortical Flows.

Abstract

Unsteady interactions of strong concentrated vortices, distributed gusts, and sharp-edged gusts with stationary airfoils have been analyzed in two-dimensional transonic flow. A simple and efficient method for introducing such vortical disturbances has been implemented in numerical codes that range from inviscid transonic small disturbance to thin-layer Navier Stokes. The numerical results demonstrate the large distortions in the overall flow field and in the surface air loads that are produced by various vortical interactions. The results of the different codes are in excellent qualitative agreement, but, as might expected, the transonic small-disturbance calculations are deficient in the important region near the leading edge. Keywords include: Gusts, Vortex interaction, Unsteady transonic flow, and Computational aerodynamics.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1984
Accession Number
ADA152417

Entities

People

  • G. R. Srinivasan
  • W. J. Mccroskey

Organizations

  • Ames Research Center

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airfoils
  • Boundary Layer
  • Computational Fluid Dynamics
  • Equations
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Free Stream
  • Layers
  • Leading Edges
  • Mach Number
  • Shock Waves
  • Stratified Fluids
  • Three Dimensional
  • Transonic Flow
  • Two Dimensional

Fields of Study

  • Physics

Readers

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