Similitude Properties of High Speed Laminar and Turbulent Boundary Layer Incipient Separation.

Abstract

Following a brief review of existing experimental knowledge about the important parameters in influencing high speed boundary layer separation, a systematic analysis is made of the various similitude rules pertaining to incipient separation including viscous-inviscid interaction for both laminar and turbulent flows. For supersonic and hypersonic turbulent flows a new scaling rule is derived which, unlike existing ones, agrees with the general trend of experimental data at high Reynolds numbers. The corresponding lateral pressure gradient effects are also examined and shown to be significant for such turbulent flows throughout the entire speed range.

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1975
Accession Number
ADA019149

Entities

People

  • George R. Inger

Organizations

  • Virginia Tech

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Experimental Data
  • Flow
  • Fluid Mechanics
  • Layers
  • Pressure Gradients
  • Reynolds Number
  • Turbulent Boundary Layer
  • Turbulent Flow

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers