HYPERSONIC FLOW PAST AXISYMMETRIC BODIES FLYING AT AN ANGLE OF ATTACK,

Abstract

The solution of the problem of the flow of an ideal gas moving at high supersonic velocity past axisymmetric bodies at angle of attack is pre sented. The problem was solved by expanding the unknown characteristics of the flow into a series with respect to parameter epsilon (gamma 1)/(gamma 1). The problem was solved in the first approximation in quadratures. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 14, 1963
Accession Number
AD0413074

Entities

People

  • B.b. Minostsev

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Axisymmetric
  • Flow
  • Fluid Flow
  • Gas Flow
  • Hypersonic Characteristics
  • Hypersonic Flow
  • Physical Properties

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Control Systems Engineering.
  • Missile Defense Systems.

Technology Areas

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