Experimental Techniques for Analyzing the Turbulent Boundary Layer

Abstract

In this report some of the methods for analyzing the turbulent boundary layer are applied to experimental data measured in full scale flight test. The values of turbulent surface shear coefficient, C sub f, were obtained using several experimental techniques and theoretical methods. The measured boundary layer growth was very much in excess of the growth predicted by Ross' treatment of the momentum equation. The values of turbulent shear measured by Clauser's method were in good agreement with values found by Preston's method. However, the Squire and Young formula used with experimentally determined values of momentum thickness and velocity yielded values of surface shear considerably higher than either of the experimental methods. The values of surface shear obtained from the von Karman momentum equation showed erratic scatter and, in general, increasing trends toward separation.

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Document Details

Document Type
Technical Report
Publication Date
Oct 07, 1954
Accession Number
AD0053360

Entities

People

  • Joseph J. Iii Cornish

Organizations

  • Mississippi State University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airspeed Indicators
  • Boundary Layer
  • Boundary Layer Flow
  • Coefficients
  • Dynamic Pressure
  • Equations
  • Flow
  • Free Stream
  • Layers
  • Measurement
  • Pitot Tubes
  • Pressure Gradients
  • Skin Friction
  • Static Pressure
  • Turbulent Boundary Layer
  • Turbulent Flow

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.
  • Regression Analysis.