About this document
Fully-Coupled Rocket Nozzle Code by Santiago Patitucci is a document available to read on EtoBox.
This report describes a computer code (FULLNOZ) for modeling rocket nozzle flows downstream of the sonic line. The code couples nonequilibrium chemistry, gas/particle thermal dynamics, turbulent mixing across streamtubes, and turbulent boundary layers. It uses a streamtube method and finite differences to integrate the governing equations of supersonic flow. Sample calculations are shown for a Minuteman nozzle. The report also provides instructions on running the code and includes a full FORTRAN listing.
- Author
- Santiago Patitucci
- Language
- EN