Adaptive Frequency Response Calibration Method for Microphone Arrays

2020 ◽  
Vol 20 (13) ◽  
pp. 7118-7128 ◽  
Author(s):  
Rui Wang ◽  
Zhe Chen ◽  
Fuliang Yin
2017 ◽  
Vol 12 (4) ◽  
Author(s):  
Yousheng Chen ◽  
Andreas Linderholt ◽  
Thomas J. S. Abrahamsson

Correlation and calibration using test data are natural ingredients in the process of validating computational models. Model calibration for the important subclass of nonlinear systems which consists of structures dominated by linear behavior with the presence of local nonlinear effects is studied in this work. The experimental validation of a nonlinear model calibration method is conducted using a replica of the École Centrale de Lyon (ECL) nonlinear benchmark test setup. The calibration method is based on the selection of uncertain model parameters and the data that form the calibration metric together with an efficient optimization routine. The parameterization is chosen so that the expected covariances of the parameter estimates are made small. To obtain informative data, the excitation force is designed to be multisinusoidal and the resulting steady-state multiharmonic frequency response data are measured. To shorten the optimization time, plausible starting seed candidates are selected using the Latin hypercube sampling method. The candidate parameter set giving the smallest deviation to the test data is used as a starting point for an iterative search for a calibration solution. The model calibration is conducted by minimizing the deviations between the measured steady-state multiharmonic frequency response data and the analytical counterparts that are calculated using the multiharmonic balance method. The resulting calibrated model's output corresponds well with the measured responses.


2019 ◽  
Vol 9 (2) ◽  
pp. 189-196
Author(s):  
Han Yao ◽  
Danyue Ma ◽  
Junpeng Zhao ◽  
Jixi Lu ◽  
Ming Ding

2021 ◽  
pp. 997-1005
Author(s):  
Erik Verreycken ◽  
Walter Daems ◽  
Jan Steckel

Author(s):  
J. Lepicovsky

A split-fiber probe was used to acquire unsteady data in a research compressor. The probe has two thin films deposited on a quartz cylinder 200 μm in diameter. A split-fiber probe allows simultaneous measurement of velocity magnitude and direction in a plane that is perpendicular to the sensing cylinder. A calibration method was devised for a split-fiber probe, and a new algorithm was developed to decompose split-fiber probe signals into velocity magnitude and direction. The algorithm is based on the minimum value of a merit function that is built over the entire range of flow velocities for which the probe was calibrated. The new decomposition scheme is fast and robust. The split-fiber probe performance and signal decomposition was first verified in a free-jet facility by comparing the data from three thermo-anemometric probes, namely a single-wire, a single-fiber, and the split-fiber probe. The wire and single-fiber probe diameters are 5 μm and 70 μm, respectively. All three probes performed extremely well as far as the velocity magnitude was concerned. However, there are differences in the peak values of measured velocity unsteadiness in the jet shear layer. The single-wire probe indicates the highest unsteadiness level, followed closely by the split-fiber probe. The single-fiber probe indicates a noticeably lower level of velocity unsteadiness. Experiments in the NASA Low Speed Axial Compressor facility revealed similar results. The mean velocities agree within 2% of the measured velocity magnitude. The differences in the measured velocity unsteadiness are similar to the case of a free jet. A reason for these discrepancies is in the different frequency response characteristics of probes used. It follows that the single-fiber probe has the slowest frequency response. In summary, the split-fiber probe worked reliably during the entire program. The acquired data averaged in time followed closely data acquired by conventional pneumatic probes. Despite small differences among all probes used, that still need to be explained, it is believed that data acquired by the split-fiber probe can be used reliably to analyze unsteady flow phenomena in the NASA Low Speed Axial Compressor.


1967 ◽  
Vol 10 (3) ◽  
pp. 405-416 ◽  
Author(s):  
Laura Ann Wilber ◽  
Victor Goodhill

Two studies were carried out to determine the usefulness of the artificial mastoid for calibration of bone-conduction vibrators as opposed to that of the real-ear calibration technique. It was found that the artificial mastoid allows more precise comparison between vibrators than does the real-ear method. Differences in frequency response characteristics, harmonic distortion, and intensity output can readily be detected with the use of the artificial mastoid, while such comparisons appear to be less precise and more variable with the real-ear calibration method.


2006 ◽  
Vol 326-328 ◽  
pp. 1483-1486
Author(s):  
Dong Seok Oh ◽  
Young Ho Lee ◽  
Chang Hwan Shin ◽  
Tae Hyun Chun ◽  
Hyung Kyu Kim ◽  
...  

A new device for measuring an acceleration in a fuel rod has been developed. The primary purpose is to apply it to the experiments for a nuclear fuel fretting, which is caused by a fuel rod and grid interaction due to a flow-induced vibration of the rods. A bi-axial accelerationdetecting device of a cylindrical shape for an insertion into a cladding tube is designed. Two unimorph piezoelectric accelerometers of small size and for special use in a high temperature condition were attached to the housing’s inner wall of the mounting device, which were oriented perpendicularly with each other to accommodate the acceleration signal during a fretting. Verification is carried out by a displacement and a frequency response analysis. The verification results of the bi-axial acceleration-detecting device showed a good response for the amplitude and bi-directional trace. This paper mainly presents the detailed design of the bi-axial accelerationdetecting device which is developed by using the design optimization of a cylindrical type and applying it to the lower and upper plugs to sustain the device in the tube wall. The verification is carried out by a displacement analysis and a frequency response analysis. An elaboration of the development procedure, calibration method and results are also given in this paper.


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