Design of Maximum Thrust Nozzles for Gas-Particle Flows. Volume II. Computer Program Manual.
Technical rept. 15 Jul 69-31 May 71,
PURDUE UNIV LAFAYETTE IND JET PROPULSION CENTER
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A program description, description of input parameters and four sample cases for the design program used to obtain maximum thrust nozzle contours for gas-particle flows are presented. The optimization analysis and the results of certain parametric studies were presented in Volume 1 of this report. Volume 2 contains a description of the program organization and overlay structure, a description of each subroutine, a description of the input parameters and their default values, and four sample cases to illustrate the use of the design program. Author
- Computer Programming and Software
- Jet and Gas Turbine Engines