Home Simulation Software Architecture in association with Robot Frank
in development: Kernel, Nozzle, Patent Download & Documentation Resource: Script

Simulation: Converging-Diverging Nozzle Model



Exit Velocity, in relation to Expansion Ratio


γ   1.30 Tc 2500 M   16.0

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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.

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Reference

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.

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Project nGene.org® is a registered trademark.