Abstract
Similar to a conventional resonance tube, a cylindrical resonator is investigated experimentally for producing high pressure and temperature gases. A quartz pressure transducer was used to determine pressure at the center of the resonator disk and a schlieren system to observe internal and external shock waves. A peak pressure nearly 3 times the jet stagnation pressure is observed and the internal shock waves are shown to be somewhat nonsymmetric and eccentric.
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Schedule a callMore From: AIAA journal. American Institute of Aeronautics and Astronautics
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