Simulation: Converging-Diverging Nozzle Model
Exit Velocity, in relation to Expansion Ratio
|γ  ||Tc||M  |
In comparison with Rocket Science textbook
REF: Figure 4.6, 4.7, and 4.11 of "Introduction to Rocket Sience and Engineering" by Travis Taylor
In comparison with NASA Rocket Nozzle Simulator (yet)
The hemodynamic software, Project nGene.org® will have been implemented to be a flexible simulator that can produce the similar results from official NASA rocket nozzle simulator, but is originally intended for the hemodynamic applications.
NASA. "Nozzle Design: Convering-Divering (CD) Nozzle": nasa.gov/WWW/K-12/airplane/nozzled.html NASA. "Interactive Nozzle": nasa.gov/WWW/k-12/VirtualAero/BottleRocket/airplane/ienzl.html Travis Taylor. "Introduction to Rocket Science and Engineering". CRC Press. 2017.