Verification of a Three-Dimensional Turbulent Boundary-Layer Calculation Method.

Abstract

The boundary-layer calculation method which forms the subject of this verification study, involves a radically different numerical scheme and geometry-handling scheme than has been employed in earlier methods. This turbulence model incorporates the empirically modified turbulent kinetic-energy equation together with an assumed relationship between the turbulent intensity and the Reynolds shear stress. The form of this relationship, and the forms of two other empirical functions of position through the boundary layer (the dissipation length and the diffusion function), have to satisfy certain rather broad theoretical constraints but otherwise must be adjusted, by trial and error, to give the best overall agreement with experiment.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1978
Accession Number
ADA055606

Entities

People

  • John F. Nash
  • Roy M. Scruggs

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Computational Fluid Dynamics
  • Equations
  • Experimental Data
  • Incompressible Flow
  • Kinetic Energy
  • Layers
  • Mach Number
  • Measurement
  • Pressure Gradients
  • Reynolds Number
  • Shear Stresses
  • Swept Wings
  • Three Dimensional
  • Turbulent Boundary Layer
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.