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aluminum test piece ASPECT RATIO attached side attachment bubble attachment distance attachment zone bistable element calculated cavitation appearance cavitation erosion cavitation number Concordia University constant control chamber volume control flow control nozzle Control Pressure Differ D/bs decrease dimensionless Experimental Lower experimental results Figure 17 flow Qs flowmeter frequency response Harry Diamond Hayashi increase interconnecting channel interconnection line Japan jet behavior jet switching main nozzle exit mathematical model Mechanism of Oscillation mode of oscillation negative resistance nozzle exit velocity offset Okayama University order oscillation oscillation can occur output loading output port pit sizes pitting rate Pneumatic Transmission Lines power-jet pressure wave rectangular lines Reference relaxation oscillation Reynolds number RIGHT CONTROL PORT shear layer shown in Figure shows side control sonic oscillator splitter distance square wave step response sufficient to switch supply flow switch the jet systems function TERMINATING VOLUME total pressure Transient Response Wada wall attachment amplifier