A Users Manual for Computer Code Nozzle.

Abstract

A perturbation formula to describe the flow in the transonic region of an axisymmetric nozzle is combined with a computer code which calculates the flow in the supersonic region by the method of characteristics. The perturbation parameter used in the transonic analysis is the normalized radius of curvature of the nozzle throat. Instructions for running the combined code, called NOZZLE, and a tabulation of the output from a test case are included. (Authro)

Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1976
Accession Number
ADA028971

Entities

People

  • John F. Polk

Organizations

  • Ballistic Research Laboratory

Tags

DTIC Thesaurus Topics

  • Axisymmetric
  • Computers
  • Curvature
  • Geometric Forms
  • Geometry
  • Instructions
  • Lines (Geometry)
  • Mathematical Analysis
  • Mathematics
  • Method Of Characteristics
  • Numerical Analysis
  • Perturbations

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Computer Science.

Technology Areas

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