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8 中国测试 2016年7月 [14 HOROWITZ S, CHEN T, CHANDRASEKHARAN V, [27 APPUKUTTAN A, SHYY W, SHEPLAK M, et al et al. A micromachined geometric moire interferometric Mixed convection induced by MEMS -based thermal floating element shear stress sensor[C]//42th AIAA shear stress sensors[. Numerical Heat Transfer: Part A Aerospace Sciences Meeting. AlAA, 2004: 1042. Applications,2003,43(3):283-305 [15 CHEN T, MILLS D, CHANDRASEKHARAN V, et al. [28 BRUSCHI P, DILIGENTI A, NAVARRINI D, et al a double Optical miniaturization of a MEMS-based floating ele- heater integrated gas flow sensor with thermal feedbacHJI ment shear stress sensor with moire amplification(Cl/ Sensors and Actuators A: Physical, 2005, 123: 210-215 48th AlAA Aerospace Sciences M AAA, 2010: 1-29 FALCO C, LUCA D A, SARFRAZ S, et al. 3D Mul- [16 CHEN T A, MILLS D, CHANDRASEKHARANV, et al. wall shear stress sensor[J]. Procedia Engineering, 201 A miniaturized optical package for wall shear stress (87):628-631 measurements in harsh environments[C]//SPIE Sensing [30] LUCA D A, HANEEF I, COULL J D, et al. High Technology+ Applications Intemational Society for Optics sensitivity single thermopile SOl CMOS MEMS thermal and photonics,2014:91130G-91130G-16. wall shear stress sensor[C]//IEEE on Sensors Journal. [17 MILLS D, CHEN T A, SHEPLAK M. Characterization Chicago:IEEE,2015,15(10):5561-5568 of an Optical Moire Wall Shear Stress Sensor for Harsh [31] RUEDI J D, NAGIB H, OSTERLUND J, et al. Evalu Environments[C]/53rd AIAA Aerospace Sciences Meet- ation of three techniques for wall-shear measurements in ing.AIAA,2015:1900-1917 three-dimensional flows[J]. Experiments in Fluids, 2003 [18 MERITT, RYAN J. Direct Measurements of Skin Fric- (5):389-396 tion at AEDC Hypervelocity Wind Tunnel9Cl∥53rd[32]杨少华,马炳和微型热敏剪应力传感器的温度补偿门 AlAA Aerospace Sciences Meeting. AIAA, 2015: 25-37 仪表技术与传感器,2011(9):9-1 [19 MERITT, RYAN J Error Source Studies of Direct Mea 33 HUGHES C, DUTTA D, BASHIRZADEH Y, et al. surement Skin Friction Sensor[C]//53rd AIAA Aerospace measuring shear stress with A Micro Fluidic sensor to Sciences meeting. AIAA2015.97-111 improve aerodynamic efficiency[C]//53rd AIAA Aerospace 20 SCHOBER M, OBERMEIER E, PIRSKAWETZ S, et al. Sciences Meeting. AlAA, 2015: 1919. A MEMS skin-friction sensor for time resolved measure [34 KJEANG E, ROESCH B, MCKECHNIE J, et al Integrated ments in separated flows[J. Experiments in Fluids, 2004 electrochemical velocimetry microfluidic devices[J] 6(4):593-599 [21 SCHIFFER M, OBERMEIER E, GREWE F, et al. [35] BRUCKER C, SPATZ J, SCHRODER WFeasability Aeromems surface fence for wall shear stress measure- study of wall shear stress imaging using microstructured ments in turbulent flows[C]//Proceedings of 44th AIAA surfaces with flexible micropillars[J]. Experiments in Aerospace Sciences Meeti nd Exhibit. AlAA. 2006 Fluids,2005,39(2):464-474 [36] BRUCKER C, BAUER D, CHAVES H. Dynamic re- 22 SAVELSBERG R, SCHIFFER M, OBERMEIER E, et al. Calibration and use of a MEMs surface fence for wall all-shear-stress[J). Experiments in Fluids, 2007, 42(5) shear stress measurements in turbulent flows[J]. Experi- 737-749 ments in Fluids,2012,53(2):489-498. [37] GROBE S, SOODT T, SCHRODER W. Dynamic cali- [23]马骋宇,马炳和,孙海浪,等.面向壁面剪应力测量的底层 bration technique for the micro-pillar shear-stress sensor 隔板微敏感结构设计与制造门航空学报,2013,34(4) MPS3 J Measurement Science and Technology, 2008 963-969 19(10):105-201 24]MA B H, MA C Y. A MEMS surface fence for wall [38] GNANAMANICKAM E P, NOTTEBROCK B, GROBE S shear stress measurement with high sensitivity[J]. Mi- et al. measurement of turbulent wall shear-stress usin crosystem Technologies, 2015(2): 1-8 micro-pillars [1. Measurement Science and Technology [25 HO C M, TAI Y C. Micro-electro-mechanical-systems 2013,24(12):124002 (MEMS)and fluid flows[]). 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