Accession Number:

ADA028971

Title:

A Users Manual for Computer Code Nozzle.

Descriptive Note:

Memorandum rept.,

Corporate Author:

BALLISTIC RESEARCH LABS ABERDEEN PROVING GROUND MD

Personal Author(s):

Report Date:

1976-08-01

Pagination or Media Count:

45.0

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

Subject Categories:

  • Computer Programming and Software
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE