EFFECTS OF TRANSPIRATION THROUGH ANGLED SLOTS ON THE DEVELOPMENT OF THE TURBULENT BOUNDARY LAYER

Abstract

An attempt was made to fundamentally understand the nature of slot transpiration and to establish an appropriate mathematical formulation of the problem suitable for its solution. These solutions will be compared with experimental data obtained at flight Reynolds numbers.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1964
Accession Number
AD0607657

Entities

People

  • Gordon Leonard Harris

Organizations

  • Mississippi State University

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Boundary Layer Flow
  • Experimental Data
  • Flow
  • Fluid Dynamics
  • Friction
  • Gliders
  • Government Procurement
  • Integral Equations
  • Pressure Distribution
  • Pressure Gradients
  • Reynolds Number
  • Skin Friction
  • Static Pressure
  • Three Dimensional
  • Transportation
  • Turbulent Boundary Layer

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Systems Analysis and Design