Instability of Flow in a Streamwise Corner

Abstract

The linear stability of an incompressible laminar flow in the blending boundary layer between the boundary layer in a 900 streamwise corner and a Blasius boundary layer well away from the corner is examined using a locally parallel flow approximation. It is shown that the influence of the outer boundary conditions associate with oblique modes of disturbances which are anti- symmetric about the bisector plane have a profound effect on the stability of the flow. As a result, in good agreement with observation, the critical streamwise Reynolds number, associated with a spanwise location is significantly reduced as the corner is approached, being R sub cr = 60 approximately for spanwise distance of Z* = 6x*/R from the corner compared with R sub cr = 322 approximately for Z* = 20x*/R solid star R-1, where X* measures downstream distance from the leading edges. At R=600, the growth rate of the most amplified mod of disturbance at the former location is over six times greater than that at the latter; the corresponding wave angle at the two locations is respectively 44 deg and 5 deg, approximately.... Corner flow, Stability.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1992
Accession Number
ADA261637

Entities

People

  • Manhar R. Dhanak

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautics
  • Blending
  • Boundaries
  • Boundary Layer
  • Boundary Layer Flow
  • Engineering
  • Equations
  • Flow
  • Fluid Dynamics
  • Laminar Flow
  • Layers
  • Poiseuille Flow
  • Reynolds Number
  • Secondary Flow
  • Steady Flow
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.