INFLUENCE OF THE LAMINAR BOUNDARY LAYER IN THE FLOW PAST A THIN BLUNTED CONE AT HIGH SUPERSONIC VELOCITIES,

Abstract

In the flight of thin blunted bodies in the atmosphere at great altitudes, an influence on the distribution of the pressure over the generatrices is exerted by the blunting and also by the thickened boundary layer. This influence is examined by the method of small disturbances with high flight Mach numbers.

Document Details

Document Type
Technical Report
Publication Date
Apr 18, 1966
Accession Number
AD0640729

Entities

People

  • I. N. Murzinov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Altitude
  • Atmospheres
  • Boundaries
  • Boundary Layer
  • Laminar Boundary Layer
  • Layers
  • Mach Number
  • Motion
  • Physical Properties

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow