About this document
Supersonic Flow in a Nozzle Simulation by Jorge A. Káram is a document available to read on EtoBox.
The document describes setting up a simulation of compressible flow through a converging-diverging nozzle in ANSYS Fluent. Key steps include: 1) Creating the axisymmetric nozzle geometry based on given area-distance data and importing coordinates; 2) Generating a mesh on the nozzle surface; 3) Defining the ideal gas model, operating conditions like stagnation pressure and temperature at the inlet, and boundary conditions like pressure at the inlet and outlet; 4) Setting reference values to non-dimensionaliz
- Author
- Jorge A. Káram
- Language
- EN