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Investigations of High Pressure Acoustic Waves in Resonators with Seal-like FeaturesA conical resonator (having a dissonant acoustic design) was tested in four configurations: (1) baseline resonator with closed ends and no blockage, (2) closed resonator with internal blockage, (3) ventilated resonator with no blockage, and (4) ventilated resonator with an applied pressure differential. These tests were conducted to investigate the effects of blockage and ventilation holes on dynamic pressurization. Additionally, the investigation was to determine the ability of acoustic pressurization to impede flow through the resonator. In each of the configurations studied, the entire resonator was oscillated at the gas resonant frequency while dynamic pressure, static pressure, and temperature of the fluid were measured. In the final configuration, flow through the resonator was recorded for three oscillation conditions. Ambient condition air was used as the working fluid.
Document ID
20040031572
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Daniels, Christopher
(NASA Glenn Research Center Cleveland, OH, United States)
Steinetz, Bruce
(NASA Glenn Research Center Cleveland, OH, United States)
Finkbeiner, Joshua
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Acoustics
Report/Patent Number
E-14336
Meeting Information
Meeting: NASA Seal/Secondary Air Flow Systems Workshop
Location: Cleveland, OH
Country: United States
Start Date: November 5, 2003
End Date: November 6, 2003
Funding Number(s)
WBS: WBS 22-708-28-15
CONTRACT_GRANT: NCC3-840
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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