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Toward a High-Frequency Pulsed-Detonation ActuatorThis paper describes the continued development of an actuator, energized by pulsed detonations, that provides a pulsed jet suitable for flow control in high-speed applications. A high-speed valve, capable of delivering a pulsed stream of reactants a mixture of H2 and air at rates of up to 1500 pulses per second, has been constructed. The reactants burn in a resonant tube and the products exit the tube as a pulsed jet. High frequency pressure transducers have been used to monitor the pressure fluctuations in the device at various reactant injection frequencies, including both resonant and off-resonant conditions. Pulsed detonations have been demonstrated in the lambda/4 mode of an 8 inch long tube at approx. 600 Hz. The pulsed jet at the exit of the device has been observed using shadowgraph and an infrared camera.
Document ID
20080013581
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cutler, Andrew D.
(George Washington Univ. Newport News, VA, United States)
Drummond, J. Philip
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2006
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA 2006-0555
LAR-16967-1
Report Number: AIAA 2006-0555
Report Number: LAR-16967-1
Funding Number(s)
WBS: WBS 599489.02.07.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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