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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Metadata
Work Title | Incompressible Center-Bore Hybrid Rocket |
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Subtitle | Velocity Ratio = 50 |
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License | CC BY-NC-SA 4.0 (Attribution-NonCommercial-ShareAlike) |
Work Type | Software Or Program Code |
Deposited | July 05, 2018 |