ON THE THEORY OF STRONG INTERACTION BETWEEN A BOUNDARY LAYER AND A HYPERSONIC INVISCID FLOW,

Abstract

The purpose of the work is to construct an asymptotic solution of these equations that corresponds to uniform motion of a gas behind a shock wave that is spreading.

Document Details

Document Type
Technical Report
Publication Date
Jul 14, 1966
Accession Number
AD0646288

Entities

People

  • N. S. Matveeva
  • V. V. Sychev

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Equations
  • Flow
  • Inviscid Flow
  • Layers
  • Shock
  • Shock Waves
  • Waves

Fields of Study

  • Mathematics
  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers