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NASA NTRS · 20060004821

Toward a High-Frequency Pulsed-Detonation Actuator

Abstract

This 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 approximately 600 Hz. The pulsed jet at the exit of the device has been observed using shadowgraph and an infrared camera.

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BibTeXRIS

Cutler, Andrew D., Drummond, J. Philip. 2006-01-01. Toward a High-Frequency Pulsed-Detonation Actuator. https://ntrs.nasa.gov/citations/20060004821

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