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Modeling Plume Afterburning Shutdown With a Double-Conditioned CMC
PI Scott Martin
This project will develop the double conditioned Conditional Moment Closure (CMC) turbulent combustion model for afterburning shutdown of hypersonic rocket exhaust plumes.
This is an Army Sequential Phase II STTR program in collaboration with Reaction Systems Inc., University of Central Florida and Propulsion Systems Inc. This project will develop the double conditioned Conditional Moment Closure (CMC) turbulent combustion model for afterburning shutdown of hypersonic rocket exhaust plumes.
Researchers
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- Department
- Aerospace Engineering Department
- Degrees
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Ph.D., M.S., B.S., University of Washington-Seattle Campus
Categories: Faculty-Staff