CONCERNING THE PROBLEM OF THE FLOW OF A HYPERSONIC STREAM OF GAS AROUND A THIN BODY,

Abstract

The hypersonic flow of an ideal gas over slender bodies is discussed. The flow Mach number is assumed to be infinite and is directed along the x-axis. Nondimensional coordinates are introduced, and a boundary value problem is obtained in nondimensional form.

Document Details

Document Type
Technical Report
Publication Date
Jan 23, 1967
Accession Number
AD0653547

Entities

People

  • N. M. Monakhov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Bodies
  • Boundaries
  • Boundary Value Problems
  • Flow
  • Hypersonic Flow
  • Mach Number
  • Physical Properties
  • Slender Bodies

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion and Flow Dynamics.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)

Technology Areas

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