The conditions of the onset of aeroacoustic resonance phenomena near a plate in a gas flow in a rectangular channel are studied theoretically and experimentally in a two-dimensional formulation. The eigenfrequency as a function of the plate's chord and its position in the channel, the shape of the eigenfunctions, and the effect of the Mach number of the basic gas flow versus the eigenfrequencies and eigenfunctions and the mechanism of self-excited oscillations are determined. A mathematical model by means of which the dependence of the resonance phenomena on the geometrical parameters of the structure were performed is proposed and substantiated.
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Univ Teknol Malaysia, Malaysia Japan Int Inst Technol, Kuala Lumpur 54100, MalaysiaUniv Teknol Malaysia, Malaysia Japan Int Inst Technol, Kuala Lumpur 54100, Malaysia
Ali, Mohamed Sukri Mat
Doolan, Con J.
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Univ Adelaide, Sch Mech Engn, Adelaide, SA 5005, AustraliaUniv Teknol Malaysia, Malaysia Japan Int Inst Technol, Kuala Lumpur 54100, Malaysia
Doolan, Con J.
Wheatley, Vincent
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Univ Queensland, Sch Mech & Min Engn, Brisbane, Qld 4072, AustraliaUniv Teknol Malaysia, Malaysia Japan Int Inst Technol, Kuala Lumpur 54100, Malaysia