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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 596Review of MEMS Techniques and Applications in...

Review of MEMS Techniques and Applications in Aerodynamics Research

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Abstract:

MEMS sensors have some attractive advantages, such as low cost, small size, which help them to be widely used in wind tunnel tests. This paper presents the basic principles and sensor types of MEMS measurement and concludes the MEMS technology for wind tunnel test applications. Future research focus is also expressed.

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Mechatronics and Industrial Informatics II

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Periodical:

Applied Mechanics and Materials (Volume 596)

Pages:

532-535

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.596.532

Citation:

Cite this paper

Online since:

July 2014

Authors:

Li Tao Fan

Keywords:

Aeroacoustic Measurement, Attitude Determination, MEMS, Shear Stress, Wind Tunnel Testings

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Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

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Citation:

[1] A. Padmanabhan, M. Sheplak, K.S. Breuer and M.A. Schmidt. Micromachined sensors for static and dynamic shear-stress measurements in aerodynamic flows[C]. In: IEEE, International Conference on Solid-state Sensors and Actuators, 1997, 137-140.

DOI: 10.1109/sensor.1997.613601

[2] Nicholas Tiliakos, George Papadopoulos, Vijay Modi, etc. MEMS shear stress sensor for hypersonic aeropropulsion test and evaluation[C]. Annual ITEA Technology Review, (2006).

[3] Tu Heng-zhang, Li Jian-qiang, Ming xiao, etc. Direct measurement technique of wall shear stress using MEMS sensors in a high-speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, Vol. 22, No. 3, 2008, pp.94-98.

[4] Kenneth S. Breuer. MEMS sensors for aerodynamic measurements- the good, the bad(and the ugly)[C]. In: AIAA, Aerospace Sciences Meeting and Exhibit, (2000).

DOI: 10.2514/6.2000-251

[5] Seun K. Kahng, Corey D. Hernandez, Sussan A. Gorton, etc. MEMS sensor system development at NASA Langley Research Center for wind tunnel applications[C]. In: AIAA, Aerospace Sciences Meeting and Exhibit, (2002).

DOI: 10.2514/6.2002-257

[6] Tom D. Finley and Ping Tcheng. Model attitude measurements at NASA Langley Research Center[C]. In: AIAA, Aerospace Sciences Meeting and Exhibit, (1992).

DOI: 10.2514/6.1992-763

[7] Sibok Yu and Brett Newman. Development of a high accuracy MEMS angular measurement system for hypersonic wind tunnel facilities[C]. In: AIAA, Structures, Structural Dynamics, and Materials Conference, (2003).

DOI: 10.2514/6.2003-1966

[8] Mathew L. Rueger and John Lafferty. Demonstration of a gyro-based model attitude measurement system at the AEDC tunnel 9 test facility[C]. In: AIAA, Fluid Dynamics Conference and Exhibit, (2008).

DOI: 10.2514/6.2008-4042

[9] Bradley L. Crawford and Tom. D Finley. Improved correction system for vibration sensitive inertial angle of attack measurement devices[C]. In: AIAA, Aerospace Sciences Meeting and Exhibit, (2000).

DOI: 10.2514/6.2000-415

[10] Mark Sheplak, John M. Seiner, Kenneth S. Breuer, etc. A MEMS microphone for aeroacoustics measurements[C]. In: AIAA, Aerospace Sciences Meeting and Exhibit, (1999).

DOI: 10.2514/6.1999-606

[11] Stephen Horowitz, Toshikazu Nishida, Louis Cattafesta, etc. Development of a micromachined piezoelectric microphone for aeroacoustics applications[J]. J. Acoust. Soc. Am., Vol. 122, No. 6, 2007, pp.3428-3436.

DOI: 10.1121/1.2785040

[12] Matthew D. Williams, Benjamin A. Griffin, Tiffany N. Reagan, etc. Micromachined aluminum nitride microphone technology development[C]. In: AIAA, Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, (2012).

DOI: 10.2514/6.2012-258

[13] Mattew D. Williams, Benjamin A. Griffin, Tiffany N. Reagan, etc. An AIN MEMS piezoelectric microphone foe aeroacoustic applictions[J]. Journal of Microelectromechanical Systems, Vol. 21, No. 2, 2012, pp.270-283.

DOI: 10.1109/jmems.2011.2176921

[14] Robert D. White, Joshua Krause, Richard De Jong, etc. MEMS microphone array on a chip for turbulent boundary layer measurements[C]. In: AIAA, Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, (2012).

DOI: 10.2514/6.2012-260

[15] J. Patrick King and James R. Underbrink. Characterization of a microelectromechanical systems(MEMS) michrophone[C]. In: AIAA, Aeroacoustics Conference, (2008).

DOI: 10.2514/6.2008-2912

[16] Shen guangping, Wu Jian, Zhang Hua, etc. Design of a 2D thermal wind sensor based on MEMS process[J]. Chinese Journal of Semiconductors, Vol. 28, No. 11, 2007, pp.1830-1835.

[17] S.D. Carnduff, S.D. Erbsloeh, A.K. Cooke, etc. Development of a low cost dynamic wind tunnel facility utilizing MEMS inertial sensors[C]. In: AIAA, Aerospace Sciences Meeting and Exhibit, (2008).

DOI: 10.2514/6.2008-196

[18] Jonathan r. Potts, Ian Lunnon, William J. Crowther, etc. Development of a transonic wind tunnel test bed for flow control actuators and sensors[C]. In: AIAA, Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, (2009).

DOI: 10.2514/6.2009-319