TY - GEN
T1 - Duct spinning mode's particle velocity imaging with in-duct circular microphone array
AU - Wei, Qingkai
AU - Chen, Bao
AU - Huang, Xun
PY - 2014
Y1 - 2014
N2 - Nowadays, the measurements within a duct have to be conducted using in-duct microphone array, which is unable to provide information of complete acoustic solutions across the test section. In this work, an imaging method of acoustic spinning modes propagating within a circular duct simply with surface pressure informa- tion is introduced. The proposed method is developed in a theoretical way and is demonstrated by a numerical simulation case. The fundamental idea behind the testing method was originally developed in control theory for ordinary differential equations. Spinning mode propagation, however, is formulated in partial differential equations. A finite difference technique is used to reduce the associated partial differential equations to a clas- sical form in control theory. The observer method can thereafter be applied straightforwardly. The algorithm is recursive and thus could be operated in real-time. The observer error of the method is analyzed then. A numerical simulation for a straight circular duct is conducted. The acoustic solutions on the test section can be reconstructed with a good agreement to analytical solutions. The results suggest the potential and applications of the proposed method.
AB - Nowadays, the measurements within a duct have to be conducted using in-duct microphone array, which is unable to provide information of complete acoustic solutions across the test section. In this work, an imaging method of acoustic spinning modes propagating within a circular duct simply with surface pressure informa- tion is introduced. The proposed method is developed in a theoretical way and is demonstrated by a numerical simulation case. The fundamental idea behind the testing method was originally developed in control theory for ordinary differential equations. Spinning mode propagation, however, is formulated in partial differential equations. A finite difference technique is used to reduce the associated partial differential equations to a clas- sical form in control theory. The observer method can thereafter be applied straightforwardly. The algorithm is recursive and thus could be operated in real-time. The observer error of the method is analyzed then. A numerical simulation for a straight circular duct is conducted. The acoustic solutions on the test section can be reconstructed with a good agreement to analytical solutions. The results suggest the potential and applications of the proposed method.
UR - https://www.scopus.com/pages/publications/85087191062
U2 - 10.2514/6.2014-3112
DO - 10.2514/6.2014-3112
M3 - Conference Paper published in a book
AN - SCOPUS:85087191062
SN - 9781624102851
T3 - 20th AIAA/CEAS Aeroacoustics Conference
BT - 20th AIAA/CEAS Aeroacoustics Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 20th AIAA/CEAS Aeroacoustics Conference 2014
Y2 - 16 June 2014 through 20 June 2014
ER -