EFFETS DE PAROI SUR UNE AILE AVEC SOUFFLAGE (EFFECTS OF A WALL ON A WING WITH BLOWING AT THE TRAILING EDGE),

Abstract

The report, relating to blowing at the trailing edge in the presence of a wall, consists of two parts. In the first part, the possibilities of calculating the potential flow are examined, and two examples are dealt with, in which the profile and the jet are replaced by a line of velocity discontinuity, where the inclination of the jet is not necessarily small. The calculation is performed by rheoelectrical analogy. The second part concerns tests making visible the flow of water at low velocities over a wing with a jet normal to the plane of the chord. Subject to the laws of similarity, these tests permit the mechanism of the flow and the effect of the principal parameters to be determined. The development of the stagnation point observed during these tests agrees well with the results of a simple calculation made in the first part. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1959
Accession Number
AD0661949

Entities

People

  • H. Werle
  • R. Duguenne

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Discontinuities
  • Dynamics
  • Flow
  • Fluid Dynamics
  • Fluid Mechanics
  • Physics
  • Potential Flow
  • Stagnation Point
  • Trailing Edges

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Fluid Dynamics.
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.