Accession Number:

AD0736820

Title:

Three-Dimensional Nozzle Design for Maximum Thrust. Volume II. Computer Program Manual.

Descriptive Note:

Technical rept. 1 Sep 66-1 Sep 71,

Corporate Author:

PURDUE UNIV LAFAYETTE IND JET PROPULSION CENTER

Personal Author(s):

Report Date:

1971-12-01

Pagination or Media Count:

56.0

Abstract:

The problem of designing three-dimensional nonaxisymmetric supersonic nozzles which produce the maximum axial thrust for a prescribed upstream flow field, mass flow rate, exit lip shape and position, and ambient pressure has been formulated and numerically solved. The formulation was written to consider a three-dimensional, supersonic, isoenergetic, homentropic flow of a perfect gas. This volume contains a description of the computer program organization and overlay structure, a description of each main program and each subroutine, a description of the input parameters, and the input listing and selected output for a sample case to illustrate the use of the design programs. Author

Subject Categories:

  • Computer Programming and Software
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE