COMPUTATION OF THE LAMINAR COMPRESSIBLE BOUNDARY LAYER.

Abstract

The report contains abstracts of significant research papers developed on the laminar compressible boundary layer in the stagnation-point region for an axisymmetric blunt body, second-order boundary layer effects in hypersonic flow past axisymmetric blunt bodies, two-dimensional hypersonic stagnation flow at low Reynolds numbers, and a numerical solution for the laminar wake behind a finite flat plate. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1969
Accession Number
AD0688888

Entities

People

  • Irmgard Flugge-lotz

Organizations

  • Stanford University

Tags

DTIC Thesaurus Topics

  • Axisymmetric
  • Blunt Bodies
  • Bodies
  • Boundaries
  • Boundary Layer
  • Flow
  • Fluid Dynamics
  • Hypersonic Flow
  • Layers
  • Reynolds Number
  • Stagnation Point
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers