Incompressible Center-Bore Hybrid Rocket

OpenFOAM simulation source files necessary to simulate the internal flow of a hybrid rocket. The attached zip file contains the directory structure which follows the normal OpenFOAM format and may be described as follows: System folder: Contains solver settings and mesh generation dictionaries Constant folder: Contains fluid and turbulence settings 0 folder: Contains boundary conditions for the steady flow problem

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Work Title Incompressible Center-Bore Hybrid Rocket
Subtitle Velocity Ratio = 50
Access
Open Access
Creators
  1. BRIAN ALLEN MAICKE
  2. ANTHONY JEAN GLUSKO
Keyword
  1. OpenFOAM
  2. hybrid rocket
  3. simulation
  4. CFD
License Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)
Work Type Software Or Program Code
Deposited July 05, 2018

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Version 1
published

  • Created
  • Added hybrid50.zip
  • Added Creator BRIAN ALLEN MAICKE
  • Added Creator ANTHONY JEAN GLUSKO
  • Published