FLOW IN A DELAVAL NOZZLE BY THE GARABEDIAN METHOD.

Abstract

The problem of computing the flow in a deLaval nozzle when an initial velocity is specified along the axis of symmetry is considered. Fortran II programs are presented for computing the flow pattern in the subsonic region, for extrapolating the data to the sonic line, for extrapolating from the sonic line into the supersonic region, and for extending the computation into the supersonic region. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1966
Accession Number
AD0631401

Entities

People

  • John V. Armitage

Tags

DTIC Thesaurus Topics

  • Computations
  • Laval Nozzles
  • Mathematical Analysis
  • Nozzles
  • Symmetry

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow