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RESEARCH OVERVIEW


PROGRAM HIGHLIGHTS AND ACHIEVEMENTS
  • High-speed shadowgraph visualization of detonation exhaust plumes
  • Optimized ejector thrust augmentation through variation of geometric parameters
  • Showed comparable turbine isentropic efficiencies resulting from steady deflagration and unsteady detonation-based combustion
GRANTS AND PARTNERSHIPS
  • GE/GRC
  • AFRL
  • Boeing Phantom Works
RESEARCH CONTACT
Ephraim Gutmark
ephraim.gutmark@uc.edu
Gas Dynamics and Propulsion Laboratory
University of Cincinnati
Dept. of Aerospace Engineering and Engineering Mechanics
300 Rhodes Hall
Cincinnati, OH 45221-0070
© 2005 University of Cincinnati