1995
DOI: 10.1016/0924-4247(94)00880-q
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Small piezoresistive silicon microphones specially designed for the characterization of turbulent gas flows

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Cited by 22 publications
(15 citation statements)
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“…Gad-el-Hak and Bandyopadhyay (1994) studied the Reynolds number effects on viscous boundary layers and concluded that to get effective results for turbulence measurements, the sensors need to be of the order of the viscous sublayer thickness, which is approximately 5 wall units. Kälvesten et al (1995) designed and fabricated piezoresistive transducers for turbulent gas flow measurements. They verified the ability of the transducer to measure the pressure eddies of 0.3-0.9 μ V/Pa in a turbulent boundary layer for different diaphragm sizes of 100 and 300 μ m. Acoustic sensors were used for turbulent gas flow measurement and its sensitivity relation with diaphragm side length was discussed.…”
Section: Aerospace Applicationsmentioning
confidence: 99%
“…Gad-el-Hak and Bandyopadhyay (1994) studied the Reynolds number effects on viscous boundary layers and concluded that to get effective results for turbulence measurements, the sensors need to be of the order of the viscous sublayer thickness, which is approximately 5 wall units. Kälvesten et al (1995) designed and fabricated piezoresistive transducers for turbulent gas flow measurements. They verified the ability of the transducer to measure the pressure eddies of 0.3-0.9 μ V/Pa in a turbulent boundary layer for different diaphragm sizes of 100 and 300 μ m. Acoustic sensors were used for turbulent gas flow measurement and its sensitivity relation with diaphragm side length was discussed.…”
Section: Aerospace Applicationsmentioning
confidence: 99%
“…Another design with the same sensing mechanism as that of [54] has been proposed in [56] with a measured resonant frequency of 16 kHz. Piezoresistive microphones can be found in applications of fluidic mechanics [57,58] and aeroacoustics [52,59].…”
Section: Piezoresistive Microphonesmentioning
confidence: 99%
“…where R is the resistance of each of the four resistors, G par is the longitudinal gauge factor, G per is the transverse gauge factor and the longitudinal strain of the resistor is assumed to dominate the contribution of the resistance change [18]. 6) and table 1.…”
Section: Theorymentioning
confidence: 99%