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

  • Scott Montgomery Martin

    Scott Montgomery Martin

    Department
    Aerospace Engineering Department
    Degrees
    Ph.D., M.S., B.S., University of Washington-Seattle Campus