METHOD OF NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW OF A GAS AROUND CONICAL BODIES,

Abstract

In this paper, a method of approximate solution and some results of calculations of a boundary value problem concerning the supersonic flow of an ideal gas around smooth conical bodies are considered. The reverse of this method is based on the multiple solution of a Cauchy problem with consecutive correction of analytically given initial data until the satisfaction with given accuracy of the boundary conditions on a given body. The results of the calculations are compared with data of calculations made by other methods and with experiments. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 28, 1964
Accession Number
AD0619564

Entities

People

  • V. F. Syagaev

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Accuracy
  • Bodies
  • Boundaries
  • Boundary Value Problems
  • Cauchy Problem
  • Conical Bodies
  • Flow
  • Supersonic Flow

Fields of Study

  • Mathematics

Readers

  • Calculus or Mathematical Analysis
  • Combustion and Flow Dynamics.
  • Operations Research

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight