BOUNDARY LAYER ON A CONTINUOUS MOVING PLANE SURFACE (O POGRANICHNOM SLOE NA DVIZHUSHCHEISYA NEPRERYVNOI PLOSKOI POVERKHNOSTI),

Abstract

The paper sets forth a solution to the equations of a plane boundary layer of compressible gas for nonlinear temperature dependence of the viscosity coefficient, as obtained with static electric integrators. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 20, 1967
Accession Number
AD0669313

Entities

People

  • A. T. Lukyanov
  • I. I. Ibragimov
  • V. P. Kashkarov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Coefficients
  • Equations
  • Integrators
  • Layers
  • Viscosity

Readers

  • Combustion and Flow Dynamics.
  • Control Systems Engineering.
  • Information Retrieval