TY - GEN
T1 - Scattering to higher harmonics for quarter wave and helmholtz resonators
AU - Förner, K.
AU - Tournadre, J.
AU - Martínez-Lera, P.
AU - Polifke, W.
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - The nonlinear response of acoustic resonators is investigated over a broad range of fre-quencies and amplitudes. Helmholtz resonators with a symmetric and with an asymmetric neck, respectively, as well as quarter wave resonators are considered. Describing functions for impedance and reection coefficient of a Helmholtz resonator at various sound pressure levels are determined from compressible flow simulation and validated against experimen-tal data. The particular focus of the present study is the nonlinear scattering to higher harmonics. For the Helmholtz resonator with a symmetric neck, a distinct pattern in the amplitudes of the higher harmonics is observed, where the odd harmonics dominate the response, while the even harmonics are almost negligible. Such an \Odd-Harmonics-Only" (OHO) pattern, which was observed previously in experiment at oriffces, can be explained by a quasi-steady analysis based on the Bernoulli equation, assuming a symmetric flow pattern at the neck. For the Helmholtz resonator with an asymmetric neck, it is observed in CFD simulations that even harmonics contribute noticeably to the resonator response, such that the OHO pattern is less pronounced. For the markedly asymmetric geometry of the quarter wave resonator, the second harmonic is dominant and the OHO pattern vanishes completely. The quasi-steady analysis is extended successfully to describe also nonlinear scattering to higher harmonics for asymmetric conffgurations and flow patterns. Overall, the scattering to higher harmonics remains on a moderate level even at very high excitation levels for the Helmholtz resonator conffgurations. For the quarter wave res- onator, the scattering is more pronounced and contributes perceptibly to the response at high excitation amplitudes.
AB - The nonlinear response of acoustic resonators is investigated over a broad range of fre-quencies and amplitudes. Helmholtz resonators with a symmetric and with an asymmetric neck, respectively, as well as quarter wave resonators are considered. Describing functions for impedance and reection coefficient of a Helmholtz resonator at various sound pressure levels are determined from compressible flow simulation and validated against experimen-tal data. The particular focus of the present study is the nonlinear scattering to higher harmonics. For the Helmholtz resonator with a symmetric neck, a distinct pattern in the amplitudes of the higher harmonics is observed, where the odd harmonics dominate the response, while the even harmonics are almost negligible. Such an \Odd-Harmonics-Only" (OHO) pattern, which was observed previously in experiment at oriffces, can be explained by a quasi-steady analysis based on the Bernoulli equation, assuming a symmetric flow pattern at the neck. For the Helmholtz resonator with an asymmetric neck, it is observed in CFD simulations that even harmonics contribute noticeably to the resonator response, such that the OHO pattern is less pronounced. For the markedly asymmetric geometry of the quarter wave resonator, the second harmonic is dominant and the OHO pattern vanishes completely. The quasi-steady analysis is extended successfully to describe also nonlinear scattering to higher harmonics for asymmetric conffgurations and flow patterns. Overall, the scattering to higher harmonics remains on a moderate level even at very high excitation levels for the Helmholtz resonator conffgurations. For the quarter wave res- onator, the scattering is more pronounced and contributes perceptibly to the response at high excitation amplitudes.
UR - http://www.scopus.com/inward/record.url?scp=85057293929&partnerID=8YFLogxK
U2 - 10.2514/6.2016-2968
DO - 10.2514/6.2016-2968
M3 - Conference contribution
AN - SCOPUS:85057293929
SN - 9781624103865
T3 - 22nd AIAA/CEAS Aeroacoustics Conference, 2016
BT - 22nd AIAA/CEAS Aeroacoustics Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 22nd AIAA/CEAS Aeroacoustics Conference, 2016
Y2 - 30 May 2016 through 1 June 2016
ER -