Design and adjustment tests of an extremely low speed calibration facility for anemometers
-
摘要:
针对极低风速情形热线风速仪标定精度不够高,且标定易受温湿度变化污染的难点问题,设计了一座速度控制精度较高、同时能控制空气温湿度的极低风速标定装置。装置的速度范围为0.1~1.0 m/s,温度范围为常温~60 ℃,湿度范围为20%RH~80%RH。进行了布局形式论证、结构设计、部件设计;设计了运动速度控制系统、温湿度控制系统,并进行了调试。调试结果表明:速度控制最大误差和最大相对误差分别为
0.000989 m/s和0.241%,达到设计指标0.003 m/s和0.4%,优于国际最优精度0.02 m/s和0.5%(风洞类)、0.001 m/s和0.82%(探头运动型);温度控制最大误差为0.9 ℃,达到设计指标1 ℃;湿度控制误差为2.9%RH,达到设计指标4%RH。将标定装置应用于某热线风速仪的标定,标定结果的拟合曲线最大误差为0.02236 m/s,满足标定精度设计指标0.03 m/s,处于国际风洞类标定装置误差范围0.018~0.03377 m/s内,接近国际探头运动型装置误差0.014 m/s;拟合曲线最大相对误差为5.214%,接近国际风洞类标定装置误差4%,接近国际探头运动型装置误差2.42%~15.04%的下限。标定装置的速度不确定度估计为0.0159 m/s,接近国际风洞类标定装置不确定度0.014~0.06 m/s下限和国际探头运动型标定装置不确定度0.012 m/s。Abstract:Considering the difficult problems existing in current extremely low speed calibration facilities that the calibration accuracy for anemometers is not high enough and the calibration is vulnerable to the contamination of temperature and humidity discrepancies, an extremely low speed calibration facility with high control precision of velocity was designed with air temperature and humidity being able to be controlled to required values. The facility had a velocity range of 0.1 to 1.0 m/s, an air temperature range of ambient atmospheric temperature to 60 ℃ and a humidity range of 20%RH to 80%RH. The layout arrangement was discussed. The mechanical structure and its components and accessories were designed and illustrated. The motion velocity control system and temperature and humidity control system were designed, tested and adjusted. The results of the adjustment tests showed that the maximum velocity control error and the maximum relative velocity control error were
0.000989 m/s and 0.241%, respectively, satisfying the design target error 0.003 m/s and 0.4%, better than the international optimal accuracy 0.02 m/s and 0.5% (wind tunnel type), and 0.001 m/s and 0.82% (probe-moving type); the maximum temperature control error was 0.9 ℃, meeting the design target error 1 ℃. The maximum humidity control error was 2.9%RH, less than the design target error 4%RH. When the facility was applied to the calibration of a hot-wire anemometer, the maximum error of the fitting curves of the calibration results was0.02236 m/s, which satisfied the design target accuracy 0.03 m/s and was within 0.018—0.03377 m/s, the error range of the international wind tunnel calibration facilities, and close to 0.014 m/s, the error of the international probe-moving facilities; the maximum relative error of fitting curves was 5.214%, close to 4%, the error of the international wind tunnel calibration facilities and close to the lower limit of 2.42%—15.04%, the international probe-moving facilities. The estimated velocity uncertainty of the facility was about0.0159 m/s, close to the lower limit of 0.014—0.06 m/s, the uncertainty of the international wind tunnel calibration facilities, and close to 0.012 m/s, the uncertainty of the international probe-moving calibration facilities. -
表 1 各国极低风速标定装置速度控制和标定性能一览
Table 1. Velocity control and calibration characteristics of world-wide extremely low speed calibration facilities
国家、机构 类型 风速范围/
(m/s)速度控制精度 速度不确定度 标定误差(不确定度) 美国NISTDTSWT 低速风洞 0.15~75 总体误差:±4% 美国NISTLVF 低速风洞 0.05~11.2 平均速度总
不确定度:1%法国CETIAT 温湿度可调风洞 0.05~2 总体不确定度:0.003~0.014 m/s 德国PTB 低速风洞 0.1~60 西班牙INTA 低速风洞 0~60 比利时UCL 开口风洞 0.3~60 1% 英国诺丁汉特伦特大学 温度可调射流风洞 0.7~9 0.5% 瑞典Gävle大学 热风洞 0.3~3 ±0.02 m/s 阿根廷国立拉普拉塔大学 直流风洞 0.2~1.25 扩展不确定度:
0.06 m/s (<10%)中国科学院大气物理所 气象风洞 0.15~22 标准误差:2.6%~7.4% 中国气象科学研究院
计量所低速风洞 0.1~2.4 中国计量科学研究院 低速风洞 0.1~1 不确定度:
0.018 m/s中国计量科学研究院 射流风洞 0.13~1.43 扩展不确定度: 0.0114 ~0.03377 m/s
(k=2)伊朗IROST* 热射流风洞 5~60 土耳其加齐安泰普大学 层流管流装置 0.029~1.79 拟合曲线标定
误差:±4%土耳其加齐安泰普大学 旋转圆盘 0.05~1.05 拟合曲线标定
误差:±5%新加坡南洋理工大学 导轨小车 0~0.35 ±0.001 m/s (−3.0%~7.0%) 拟合曲线标定误差:−1.11%~15.04% 英国布莱顿理工学院 导轨小车 0.02~1 ± 0.0082 m/s (±0.82%)意大利INRIM 导轨小车 0.1~1.2 总体(扩展)不确定度:
0.012 m/s (8%)日本计量研究院力学部 导轨小车 0.05~1 不确定度: 0.00735 ~0.014 m/s中国计量科学研究院 导轨小车 0.1~1.05 扩展不确定度:
0.82% (k=2)扩展不确定度:
2.42% (k=2)加拿大渥太华大学 单摆式装置 最大速度0.3~10 意大利INRIM 水平旋转臂 0.2~5 扩展不确定度: 4.0%~0.84% 沙特法赫德国王
石油矿产大学水平摇摆臂 0~0.15 最大不确定度
(95%置信水平):
4.1%英国布莱德福德大学* 摇摆臂 1~6.5 0.03 m/s 德国埃尔朗根-纽伦堡
大学*实验气候舱 12.75~36.6 表 2 各国标定装置温湿度控制特性
Table 2. Temperature and humidity control characteristics of world-wide extremely low speed calibration facilities
国家、机构 类型 风速范围/
(m/s)温度范围/℃ 温度控制精度 湿度范围/
%RH湿度控制
精度/%RH法国CETIAT 温湿度可控风洞 0.05~2 10~50 ±0.5 ℃ (均匀性:±0.2 ℃);
达到设定温湿度需时≤ 2 h10~90 ±4(均匀性:±0.5) 英国诺丁汉特伦特大学 热射流风洞 0.7~9 20~60 0.1 ℃ 瑞典Gävle大学 热风洞 0.3~3 10~60 ±0.05 ℃ 伊朗IROST* 热射流风洞 5~30 22~60 德国埃尔朗根-
纽伦堡大学*实验气候舱 12.75~36.6 30~70 30~90 表 3 双频激光干涉仪校核结果
Table 3. Checking results of magnetic grating ruler by dual-frequency laser interferometer
测量序号 距离/mm 误差/% 干涉仪 磁栅尺 第1次 0 0 0 1001.02 1001.02 0 2002.85 2002.86 0.0005 3004.50 3004.58 0.0027 4006.50 4006.42 −0.002 5008.25 5008.21 −0.001 6010.10 6010.05 −0.001 7011.75 7011.72 0 8013.58 8013.56 0 第2次 0 0 0 1000.97 1001.01 0.004 2002.78 2002.85 0.003 3004.48 3004.59 0.004 4006.39 4006.39 0 5008.21 5008.2 0 6010.03 6010.01 0 7011.7 7011.71 0 8013.52 8013.53 0 表 4 匀速段速度控制特性(绝对误差)
Table 4. Velocity control characteristics in constant-speed stage (absolute error)
m/s Uset Uavg σU |Ui−Uavg|max |Ui−Uset|max |Uavg−Uset| 0.1 0.0999992 0.0001080 0.0002402 0.000241 0.00000080 0.2 0.1999986 0.0000663 0.0002856 0.000287 0.00000137 0.3 0.2999966 0.0000994 0.0005346 0.000538 0.00000346 0.4 0.3999942 0.0000895 0.0003118 0.000306 0.00000584 0.5 0.5000054 0.000105 0.0002704 0.000265 0.00000536 0.6 0.6000041 0.0001454 0.0003918 0.000396 0.00000411 0.7 0.7000112 0.0001750 0.0009778 0.000989 0.00001121 0.8 0.8000122 0.0001658 0.0004582 0.000446 0.00001222 0.9 0.9000024 0.0001573 0.0004504 0.000448 0.00000238 1.0 1.0000160 0.0001228 0.0003980 0.000414 0.00001597 表 5 匀速段速度控制特性(相对误差)
Table 5. Velocity control characteristics in constant-speed stage (relative error)
Uset/(m/s) (σU/Uavg)/% (|Ui−Uavg|max/Uavg)/% (|Ui−Uset|max/Uset)/% (|Uavg−Uset|/Uset)/% 0.1 0.108021 0.240201 0.241004 0.000805 0.2 0.033140 0.142814 0.143498 0.000686 0.3 0.033131 0.178190 0.179340 0.001152 0.4 0.022382 0.077957 0.076495 0.001460 0.5 0.021007 0.054073 0.053001 0.001073 0.6 0.024238 0.065306 0.065992 0.000686 0.7 0.024994 0.139686 0.141289 0.001601 0.8 0.020730 0.057279 0.055753 0.001527 0.9 0.017475 0.050041 0.049777 0.000265 1.0 0.012280 0.039803 0.041401 0.0015974 表 6 密闭室温度达到设定值所需时间和恒温保持时间
Table 6. Time required to reach the set temperature and the time in which temperature can be maintained constant
θset/℃ 名义起始温度/℃ 实际起始温度/℃ 稳定时θavg/℃ tr,θ/min tm,θ/min 30 室温 23.5 29.9±0.3 95 36.67 40 30 29.9 39.7±0.2 75 20 50 40 38.1 50.0±0.4 96.67 25 60 50 49.8 60.1±0.4 58 42 60 室温 26.9 60.1±0.4 123 21.67 表 7 密闭室温度达到设定值时的温度分布特性
Table 7. Temperature distribution characteristics in the enclosed chamber when reaching the set value
θset/℃ 起始温度/℃ θavg/℃ σθ/℃ |θi−θavg|max/℃ |θi−θset|max/℃ |θavg−θset|/℃ 30 23.5 29.9 0.1432 0.5 0.6 0.1 40 29.9 39.7 0.1364 0.4 0.7 0.3 50 38.1 50.0 0.1985 0.7 0.7 0.0 60 49.8 60.1 0.2668 0.8 0.9 0.1 60 26.9 60.1 0.2793 0.8 0.9 0.1 表 8 湿度达到设定值所需时间和恒定湿度保持时间
Table 8. Time required to reach the set humidity and time in which humidity can be maintained constant
θset /℃ Hset/%RH 起始湿度/%RH 实际起始湿度/%RH 稳定时的Havg/%RH tr,H/min tm,H/min 21.5 20 环境湿度 42.7 20.9±0.8 35.17 16.92 21.5 60 20 24 60.1±0.2 23.33 25 21.5 80 60 59.6 79.8±0.5 20.67 34.33 30 20 环境湿度 58.5 20.6±1.7 10 90 30 60 20 19.2 60.3±0.4 16.67 28.33 30 80 60 60 80.2±0.3 9.67 22.83 40 20 环境湿度 77.9 19.9±0.3 11.33 13.67 40 60 20 35.5 59.7±0.3 80 23.67 40 80 60 57.1 79.8±0.3 22.17 22.83 表 9 密闭室湿度达到设定值时的湿度分布特性
Table 9. Humidity distribution characteristics in the enclosed chamber when reaching the set value
θset/℃ Hset/%RH Havg/%RH σH/%RH |Hi−Havg|max/%RH |Hi−Hset|max/%RH |Havg−Hset|/%RH 21.5 20 20.9 0.8474 0.8 1.7 0.9 21.5 60 60.1 0.0935 0.6 0.7 0.1 21.5 80 79.8 0.1871 0.8 1.0 0.2 30 20 20.6 0.5613 2.3 2.9 0.6 30 60 60.3 0.2806 0.5 0.8 0.3 30 80 80.2 0.1871 0.3 0.5 0.2 40 20 19.9 0.0935 0.3 0.4 0.1 40 60 59.7 0.2806 0.3 0.6 0.3 40 80 79.8 0.1871 1.3 1.4 0.1 表 10 拟合曲线中的常数
Table 10. Constants in the fitting curves of modified King’s law
θset/℃ Hset/%RH a b m 30 20 1.644 0.6586 0.6344 60 1.669 0.6538 0.7074 80 1.615 0.687 0.6136 40 20 1.507 0.6467 0.5967 60 1.502 0.6710 0.5578 80 1.59 0.6047 0.6963 60 19 1.358 0.521 0.6429 表 11 各设定速度下不同温湿度条件下拟合速度与实际控制速度的误差
Table 11. Deviationerror of the fitted velocity from the real controlled velocity at each set velocity
θset/℃ Hset/
%RHΔU/(m/s) Uset=0.1 m/s Uset=0.2 m/s Uset=0.3 m/s Uset=0.4 m/s Uset=0.5 m/s Uset=0.6 m/s Uset=0.7 m/s Uset=0.8 m/s Uset=0.9 m/s Uset=1.0 m/s 30 20 0.000936 − 0.001983 0.007060 − 0.013160 − 0.001592 − 0.000700 0.014904 0.008045 − 0.004668 − 0.008005 30 60 0.005120 − 0.008284 − 0.004327 − 0.002082 0.001401 0.010295 0.001245 0.010876 0.000303 − 0.013959 30 80 0.003931 − 0.006744 − 0.007101 − 0.001695 0.007487 0.006810 0.005058 0.004932 − 0.003850 − 0.010266 40 20 0.003843 − 0.003238 − 0.007840 − 0.020857 0.011302 0.017635 0.022360 0.002771 − 0.017634 − 0.010954 40 60 0.003933 − 0.009262 0.004476 − 0.002688 − 0.003538 0.004099 0.016339 0.009140 − 0.002509 − 0.013690 40 80 0.002976 − 0.001466 − 0.004627 − 0.003603 0.006449 0.001741 − 0.002190 0.018522 0.004364 − 0.014859 60 19 0.000955 − 0.000994 0.002008 0.002485 0.000636 − 0.000445 0.000611 0.002805 0.000003 0.001691 表 12 各设定速度下拟合速度与实际控制速度的最大误差
Table 12. Maximum deviation error of the fitted velocity from the real controlled velocity at each set velocity
Uset/(m/s) |ΔU|max/(m/s) (|ΔU|max/Uset)/% 0.1 0.005120 5.12 0.2 0.009262 4.631 0.3 0.007840 2.6133 0.4 0.020857 5.2143 0.5 0.011302 2.2604 0.6 0.017635 2.9392 0.7 0.022360 3.1943 0.8 0.018522 2.3153 0.9 0.017634 1.9593 1.0 0.014859 1.4859 表 13 有无侧壁情形过杆顶中心水平线的速度差最大值
Table 13. Maximum velocity difference along the horizontal line passing through the rod top center between the case with side walls and the case without side walls
参数 支杆位置x/m 2 5 8 |ΔU|max/(m/s) 0.0085 0.0025 0.003 (|ΔU|max/U)/% 0.85 0.25 0.3 表 14 有无前端壁情形过杆顶中心水平线的速度差最大值
Table 14. Maximum velocity difference along the horizontal line passing through the rod top center between the case with front wall and the case without front wall
参数 支杆位置x/m 2 5 8 |ΔU|max/(m/s) 0.001 0.0011 0.0011 (|ΔU|max/U)/% 0.1 0.11 0.11 -
[1] 盛森芝,沈熊,舒玮. 流速测量技术[M]. 北京: 北京大学出版社,1987. SHENG Senzhi,SHEN Xiong,SHU Wei. Velocity measurement technology[M]. Beijing: Peking University Press,1987. (in ChineseSHENG Senzhi, SHEN Xiong, SHU Wei. Velocity measurement technology[M]. Beijing: Peking University Press, 1987. (in Chinese) [2] 盛森芝,徐月亭,袁辉靖. 热线热膜流速计[M]. 北京: 中国科学技术出版社,2003. SHENG Senzhi,XU Yueting,YUAN Huijing. Hot-wire hot-film anemometer[M]. Beijing: China Science and Technology Press,2003. (in ChineseSHENG Senzhi, XU Yueting, YUAN Huijing. Hot-wire hot-film anemometer[M]. Beijing: China Science and Technology Press, 2003. (in Chinese) [3] BRUUN H H,FARRAR B,WATSON I. A swinging arm calibration method for low velocity hot-wire probe calibration[J]. Experiments in Fluids,1989,7(6): 400-404. doi: 10.1007/BF00193422 [4] CHUA L P,LI H S,ZHANG H. Calibration of hot wire for low speed measurements[J]. International Communications in Heat and Mass Transfer,2000,27(4): 507-516. doi: 10.1016/S0735-1933(00)00133-0 [5] GUELLOUZ M S,TAVOULARIS S. A simple pendulum technique for the calibration of hot-wire anemometers over low-velocity ranges[J]. Experiments in Fluids,1995,18(3): 199-203. doi: 10.1007/BF00230265 [6] BALL S J,ASHFORTH-FROST S,JAMBUNATHAN K,et al. Appraisal of a hot-wire temperature compensation technique for velocity measurements in non-isothermal flows[J]. International Journal of Heat and Mass Transfer,1999,42(16): 3097-3102. doi: 10.1016/S0017-9310(98)00371-8 [7] LUNDSTRÖM H,SANDBERG M,MOSFEGH B. Temperature dependence of convective heat transfer from fine wires in air: a comprehensive experimental investigation with application to temperature compensation in hot-wire anemometry[J]. Experimental Thermal and Fluid Science,2007,32(2): 649-657. doi: 10.1016/j.expthermflusci.2007.08.002 [8] DURST F,NOPPENBERGER S,STILL M,et al. Influence of humidity on hot-wire measurements[J]. Measurement Science and Technology,1996,7(10): 1517-1528. doi: 10.1088/0957-0233/7/10/021 [9] MEASE N E,CLEVELAND W G Jr. ,MATTINGLY G E,et al. Air speed calibration at the national institute of standards and technology[R]. Anaheim,California,US: Measurement Science Conference,1991. [10] CROWLEY C,SHINDER I I,MOLDOVER M R. The effect of turbulence on a multi-hole Pitot calibration[J]. Flow Measurement and Instrumentation,2013,33: 106-109. doi: 10.1016/j.flowmeasinst.2013.05.007 [11] SHINDER I I,MOLDOVER M R,FILLA B J,et al. Facility for calibrating anemometers as a function of air velocity vector and turbulence[J]. Metrologia,2021,58(4): 045008. doi: 10.1088/1681-7575/ac0a92 [12] CARE I. Characterization of a new calibration wind-tunnel within low air velocity range[R].Guilin,China: 12th International Conference on Flow Measurement,2004. [13] SÁNCHEZ J R,MÜLLER H,CARE I,et al. Air velocity sensors’ calibration intercomparison using LDA as standards[R]. Lisbon,Portugal: 12th International Symposium on Applications of Laser Techniques to Fluid Mechanics,2004. [14] PEZZOTTI S,D’IORIO J I,NADAL-MORA V,et al. A wind tunnel for anemometer calibration in the range of 0.2–1.25 m/s[J]. Flow Measurement and Instrumentation,2011,22(4): 338-342. doi: 10.1016/j.flowmeasinst.2011.04.006 [15] 中国科学院大气物理研究所. 极低速气象标定风洞[J]. 地球科学进展,1986,1(增刊1): 84-85. Institute of Atmospheric Physics,Chinese Academy of Sciences. Very low speed meteorological calibration wind tunnel[J]. Advances in Earth Science,1986,1(Suppl. 1): 84-85. (in ChineseInstitute of Atmospheric Physics, Chinese Academy of Sciences. Very low speed meteorological calibration wind tunnel[J]. Advances in Earth Science, 1986, 1(Suppl. 1): 84-85. (in Chinese) [16] 张佩龙,苏锁群,杨云. 极低速范围风速仪的标定[J]. 气象科技,1991(2): 93-96. ZHANG Peilong,SU Suoqun,YANG Yun. Calibration of extremely low speed range anemometer[J]. Meteorological Science and Technology,1991(2): 93-96. (In ChineseZHANG Peilong, SU Suoqun, YANG Yun. Calibration of extremely low speed range anemometer[J]. Meteorological Science and Technology, 1991(2): 93-96. (In Chinese) [17] 李鹏,崔骊水,李金海,等. 热线风速仪微风速(0.1~1 m/s)下的校准实验研究[J]. 计量技术,2016(9): 3-7. LI Peng,CUI Lishui,LI Jinhai,et al. Calibration experimentof hot-wire anemometer at very low speed (0.1~1 m/s)[J]. Metrological Technology,2016(9): 3-7. (In ChineseLI Peng, CUI Lishui, LI Jinhai, et al. Calibration experimentof hot-wire anemometer at very low speed (0.1~1 m/s)[J]. Metrological Technology, 2016(9): 3-7. (In Chinese) [18] 吴琼. 热线风速仪现场校准的微风速射流装置的研究[D]. 河北 保定: 河北大学,2018. WU Qiong. Study on on-site calibration of hot-wire anemometerforbreezejetdevice[D]. Baoding Hebei: Hebei University,2018. (in ChineseWU Qiong. Study on on-site calibration of hot-wire anemometerforbreezejetdevice[D]. Baoding Hebei: Hebei University, 2018. (in Chinese) [19] ARDEKANI M A,FARHANI F. Experimental study on response of hot wire and cylindrical hot film anemometers operating under varying fluid temperatures[J]. Flow Measurement and Instrumentation,2009,20(4/5): 174-179. [20] ÖZAHI E,ÇARPıNLıOǦLU M Ö,GÜNDOǦDU M Y. Simple methods for low speed calibration of hot-wire anemometers[J]. Flow Measurement and Instrumentation,2010,21(2): 166-170. doi: 10.1016/j.flowmeasinst.2010.02.004 [21] HEIKAL M,ANTONIOU A,COWELL T A. A rig for the static calibration of constant-temperature hot wires at very low velocities[J]. Experimental Thermal Fluid Science,1988,1: 221-223. doi: 10.1016/0894-1777(88)90038-6 [22] SPAZZINI P G,PICCATO A,MALVANO R. Metrological features of the linear low-speed anemometer calibration facility at INRIM[J]. Metrologia,2009,46(1): 109-118. doi: 10.1088/0026-1394/46/1/014 [23] 日本计量研究所力学部. 日本和美国的微风速标准的比较[J]. 李小晋,译. 实用测试技术,1997(4): 48-49. Mechanics Division,Japanese National ResearchLaboratory of Metrology. Comparison of extremely low speed standards between Japan and the United States[J]. Translated by LI Xiaojin. Practical Measurement Technology,1997(4): 48-49 (In ChineseMechanics Division, Japanese National ResearchLaboratory of Metrology. Comparison of extremely low speed standards between Japan and the United States[J]. Translated by LI Xiaojin. Practical Measurement Technology, 1997(4): 48-49 (In Chinese) [24] 崔骊水,李鹏,邱丽荣,等. 微风速标准装置的建立和热线风速仪校准方法的实验研究[J]. 计量学报,2018,39(3): 289-293. CUI Lishui,LI Peng,QIU Lirong,et al. Experimentinvestigationoncalibrationofhotwireanemometerbased on lowairspeedreferencefacility[J]. Acta Metrologica Sinica,2018,39(3): 289-293. (in ChineseCUI Lishui, LI Peng, QIU Lirong, et al. Experimentinvestigationoncalibrationofhotwireanemometerbased on lowairspeedreferencefacility[J]. Acta Metrologica Sinica, 2018, 39(3): 289-293. (in Chinese) [25] PICCATO A,MALVANO R,SPAZZINI P G. Metrological features of the rotating low-speed anemometer calibration facility at INRIM[J]. Metrologia,2010,47(1): 47-57. doi: 10.1088/0026-1394/47/1/006 [26] AL-GARNI A M. Low speed calibration of hot-wire anemometers[J]. Flow Measurement and Instrumentation,2007,18(2): 95-98. doi: 10.1016/j.flowmeasinst.2007.01.003 [27] 钱政,王中宇. 误差理论与数据处理[M]. 2版. 北京: 科学出版社,2022. QIAN Zheng,WANG Zhongyu. Error theory and data processing[M]. 2nd. ed. Beijing: Science Press,2022. (in ChineseQIAN Zheng, WANG Zhongyu. Error theory and data processing[M]. 2nd. ed. Beijing: Science Press, 2022. (in Chinese) [28] TAYLOR J R. An introduction to error analysis: the study of uncertainties in physical measurements[M]. 2nd ed. Sausalito,US: University Science Books,1997. [29] 周廷波,田永强,刘佳航,等. 极低风速标定系统密闭室扰动衰减时间研究[J]. 实验力学,2022,37(5): 638-648. ZHOU Tingbo,TIAN Yongqiang,LIU Jiahang,et al. Research on disturbance attenuation time in an extremely low wind speed calibration facility[J]. Journal of Experimental Mechanics,2022,37(5): 638-648. (in ChineseZHOU Tingbo, TIAN Yongqiang, LIU Jiahang, et al. Research on disturbance attenuation time in an extremely low wind speed calibration facility[J]. Journal of Experimental Mechanics, 2022, 37(5): 638-648. (in Chinese) [30] 周廷波,田永强,刘佳航,等. 极低风速标定系统密闭室洞壁影响研究[J]. 航空工程进展,2022,13(6): 125-133. ZHOU Tingbo,TIAN Yongqiang,LIU Jiahang,et al. Research on sealed chamber wall effects in an extremely low wind speed calibration facility[J]. Advances in Aeronautical Science and Engineering,2022,13(6): 125-133. (in ChineseZHOU Tingbo, TIAN Yongqiang, LIU Jiahang, et al. Research on sealed chamber wall effects in an extremely low wind speed calibration facility[J]. Advances in Aeronautical Science and Engineering, 2022, 13(6): 125-133. (in Chinese) [31] 周廷波,王欧,张正科,等. 标定系统密闭室壁面温度差诱导流动研究[J]. 实验力学,2023,38(2): 231-242. ZHOU Tingbo,WANG Ou,ZHANG Zhengke,et al. Research on flows induced by wall temperature difference in an enclosed chamber of a calibration facility[J]. Journal of Experimental Mechanics,2023,38(2): 231-242. (in ChineseZHOU Tingbo, WANG Ou, ZHANG Zhengke, et al. Research on flows induced by wall temperature difference in an enclosed chamber of a calibration facility[J]. Journal of Experimental Mechanics, 2023, 38(2): 231-242. (in Chinese) [32] 刘佳航. 极低风速标定系统设计关键技术研究[D]. 西安: 西北工业大学,2021: 27-42. LIU Jiahang. Research on key technologies in the design of an extremely low wind speed calibration system[D]. Xi’an: Northwestern Polytechnical University,2021: 27-42. (in ChineseLIU Jiahang. Research on key technologies in the design of an extremely low wind speed calibration system[D]. Xi’an: Northwestern Polytechnical University, 2021: 27-42. (in Chinese) -

下载: