Solution of the Chaplygin Equation by the Straight-Line Method,

Abstract

The Chaplygin equation is solved in the article by the straight-line method. This solution describes a gas flow around a profile at a high subsonic speed with a local supersonic area limited by a curved shock wave. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 17, 1972
Accession Number
AD0753557

Entities

People

  • A. Ryskulov
  • I. Biibosunov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Equations
  • Flow
  • Gas Flow
  • Shock
  • Shock Waves
  • Waves

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow