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Marshall Space Flight Center
2005 Phase 3
Development of Generalized Equations of State and CFD Algorithms for Arbitrary Mixtures of Non-Ideal Fluids
Tetra Research Corporation/Mississippi State University
Princeton, IL/Starkville, MS
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INNOVATION
- Develop and evaluate thermodynamic models suitable for liquids, gases, and supercritical vapors
- Create generalized algorithms for arbitrary mixtures of non-ideal multi-phase flows
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Characteristic LOX Bump Due to Expanding Core Flow Recirculation
Can Now Be Predicted Using the Real Fluids Model
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ACCOMPLISHMENTS
- Solved problem of numerical noise in rapidly changing functions near the critical isotherm
- Improved low temperature predictions near the critical point without affecting high temperature numerical behavior
- Extended Eulerian dispersed phase capability to support two-way coupled multiphase problems, including particle composition evolution and energy coupling
- Developed initial framework for extension to Lagrangian multiphase calculations
- Provided enabling technology for application of CFD to a broader range of injector designs, including performance and environment predictions
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COMMERCIALIZATION
- Supporting ER42 (MSFC’s Fluid Dynamics Branch) with advanced liquid and solid motor analyses
- Supporting University research programs through the Constellation University Institutes Project (CUIP) activity
- Software currently in use at Purdue University
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GOVERNMENT/SCIENCE
APPLICATIONS
- Liquid engines
- Solid rocket motors
- Plume impingement
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Power/Propulsion, Aerodynamics, Aerospace, Chemistry, Cryogenic Sciences
Curator: SBIR Support 8/27/08 |