THE CALCULATION OF NONLINEAR SUPERSONIC CONICAL FLOWS BY THE METHOD OF INTEGRAL RELATIONS,

Abstract

The supersonic flow over cones of arbitrary shape was investigated by using the method of integral relations. The equations are derived for one strip using a body-oriented coordinate system. Various choices for basic equations are discussed. The solution of the boundary value problem for a number of fundamentally different cases is discussed in detail and various suggestions concerning improvements of the method and other related methods are made. Due to severe computational difficulties, however, no numerical results are presented. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1964
Accession Number
AD0605284

Entities

People

  • John W. Brock

Organizations

  • Grumman

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Value Problems
  • Cooperation
  • Coordinate Systems
  • Differential Equations
  • Equations
  • Flow
  • Integrals
  • Mathematics
  • Supersonic Flow

Fields of Study

  • Mathematics

Readers

  • Calculus or Mathematical Analysis
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers