TY - JOUR
T1 - Real-time reconstruction of unsteady rotating forces acting by rotor blades in moving medium
AU - Xu, Ying
AU - Casalino, Damiano
AU - Zhang, Xiao Zheng
AU - Zhang, Yong Bin
AU - Bi, Chuan Xing
PY - 2024
Y1 - 2024
N2 - A time-domain inverse aeroacoustic method based on the convective Ffowcs Williams–Hawkings equation is presented. The method allows to determine, in real-time, the unsteady forces exerted on rotating blades in the presence of a moving medium. The inversion procedure is based on a space-time regularization with a mixed l1,2-norm, which guarantees accuracy and smoothness of the solution. The method is initially verified through synthetic acoustic signals emitted by rotating sources in a constant flow, up to a convective Mach number of about 0.88. Then the method is validated through signals generated by a propeller immersed in a wind-tunnel jet flow, up to a Mach number of 0.06. Due to the reduced convective Mach number, the leading aeroacoustic effect is derived from a variation of the blade loading. It is argued that the onset of flow separation at high values of the rotor advance ratio is responsible for the onset of force fluctuations that the inverse method is able to retrieve both qualitatively and quantitatively.
AB - A time-domain inverse aeroacoustic method based on the convective Ffowcs Williams–Hawkings equation is presented. The method allows to determine, in real-time, the unsteady forces exerted on rotating blades in the presence of a moving medium. The inversion procedure is based on a space-time regularization with a mixed l1,2-norm, which guarantees accuracy and smoothness of the solution. The method is initially verified through synthetic acoustic signals emitted by rotating sources in a constant flow, up to a convective Mach number of about 0.88. Then the method is validated through signals generated by a propeller immersed in a wind-tunnel jet flow, up to a Mach number of 0.06. Due to the reduced convective Mach number, the leading aeroacoustic effect is derived from a variation of the blade loading. It is argued that the onset of flow separation at high values of the rotor advance ratio is responsible for the onset of force fluctuations that the inverse method is able to retrieve both qualitatively and quantitatively.
KW - Inverse aeroacoustic method
KW - Moving medium
KW - Real-time reconstruction
KW - Rotor noise
KW - Unsteady rotating forces
UR - http://www.scopus.com/inward/record.url?scp=85166472616&partnerID=8YFLogxK
U2 - 10.1016/j.jsv.2023.117972
DO - 10.1016/j.jsv.2023.117972
M3 - Article
AN - SCOPUS:85166472616
SN - 0022-460X
VL - 568
JO - Journal of Sound and Vibration
JF - Journal of Sound and Vibration
M1 - 117972
ER -