EMPLOYING THE KARMAN METHOD FOR CALCULATING A TURBULENT BOUNDARY LAYER ON A PLATE IN A GAS FLOW

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1963
Accession Number
AD0400500

Entities

People

  • L. G. Loytsanskiy
  • Yu. V. Lapin

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Boundaries
  • Boundary Layer
  • Coefficients
  • Equations
  • Experimental Data
  • Flow
  • Foreign Technology
  • Friction
  • Gas Flow
  • Government Procurement
  • Heat Transfer
  • Integral Equations
  • Integrals
  • Layers
  • Thickness
  • Turbulent Boundary Layer