INVESTIGATION OF THE BOUNDARY CONDITION AT A PERFORATED WALL

Abstract

The problem considered is that of findings a potential which will yield a constant horizontal velocity in a slot in a solid wall but no vertical velocity outside the slot. The pressure over the slot width is assumed to be constant. The problem is transformed to that of the perturbation flow field generated by a flat plate moving downward with a constant velocity. The potential of the flat plate is obtained by applying the Joukowski transformation to the flow about a cylinder. A consideration of the boundary conditions indicates that the solutions must be limited to those having a stagnation point at one edge of the slot for an appropriate solution to be obtained for the velocity distribution about the slot. A method described by Grammel (Die Hydrodynamischen Grundlagen des Fluges, Friedrich Vieweg, Braunschweig, 1917) is used to obtain the velocities produced by a wall considered as containing an infinite number of transverse slots uniformily spaced along an axis. The theoretical analysis was confirmed by experiments with a low-speed wind tunnel. As an additional experiment the influence of the initial boundary layer was determined by tests on perforated metal inserts of 1- to 5-in. lengths. The results indicated that the boundary condition for a perforated wall is linear. The Reynolds number, which varied over a large range, does not affect the linearity.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1953
Accession Number
AD0014022

Entities

People

  • Paul F. Maeder

Organizations

  • Brown University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Data Reduction
  • Dynamic Pressure
  • Flow
  • Flow Fields
  • Mach Number
  • Military Research
  • Plenum Chambers
  • Potential Flow
  • Pressure Distribution
  • Pressure Measurement
  • Reynolds Number
  • Stagnation Point
  • Transverse
  • Two Dimensional
  • United States

Readers

  • Fluid Dynamics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster