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EVALUATION OF CORRECTIONS ON TURBULENT FLUXES OBTAINED BY EDDY COVARIANCE METHOD IN HIGH WINDS 被引量:1
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作者 BI Xue-yan WEN Bin +5 位作者 ZHAO Zhong-kuo HUANG Jian LIU Chun-xia HUANG Hui-jun MAO Wei-kang WEN Guan-huan 《Journal of Tropical Meteorology》 SCIE 2018年第2期176-184,共9页
This paper investigates processing of fast-response data and corrections of turbulent fluxes obtained by using eddy covariance method based on data collected at an offshore observation tower during three Cold-intrusio... This paper investigates processing of fast-response data and corrections of turbulent fluxes obtained by using eddy covariance method based on data collected at an offshore observation tower during three Cold-intrusion(CI)events in the South China Sea in 2010. This study presents the data processing procedure in detail and compares frictional velocities(u*), sensible heat fluxes(H) and latent heat fluxes(LE) yielded by using different averaging periods and different coordinate rotation methods; evaluates the sonic temperature correction for sensible heat flux and the Webb correction for latent heat flux as a function of 10 m wind speed(u10) during the CIs. The results show(1) that the different averaging periods of 30 min and 10 min cause biases of u*(H, LE) within 5%(15%, 62%). The values of u*(H,LE) averaged from 30 mins are mostly larger than those averaged from 10 mins. We suggest that the averaging period of 10 min is not sufficiently long to capture all scale eddies and recommend 30 min averaging period in calculating turbulent fluxes using eddy covariance method during CIs;(2) that the values of u*(H, LE) obtained from double rotation(DR2) and those obtained from planar fit rotation(PF) have good agreements and correlation coefficients between them are larger than 0.99. Because PF method requires unchanged environment and it is easier to apply DR2 method, we suggest DR2 coordinate rotation method in processing fast-response data; and(3) that the median values of frictional velocity(sensible heat flux and latent heat flux) binned according to 2 m s^(-1) intervals of u_(10) increase(decrease,increase) by less than 9%(4%, 10%) by Coriolis corrections(sonic temperature corrections, Webb corrections), which decreases(decreases, increases) with increasing u10 when u10 are 5-17 m s^(-1). 展开更多
关键词 processing of fast-response data averaging period coordinate rotation Coriolis correction sonic temperature correction Webb correction
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涡轮盘用GH4706高温合金热变形行为
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作者 张森峰 杨文彬 +4 位作者 夏玉峰 杨伟 郑德宇 滕海灏 杜潇 《锻压技术》 CAS CSCD 北大核心 2024年第9期202-212,共11页
在变形温度为850~1100℃、应变速率为0.001~0.1 s^(-1)的条件下,利用Thermecmastor型热模拟试验机研究了锻态GH4706高温合金的热变形行为。综合考虑绝热温升和摩擦效应,对真应力-真应变曲线进行摩擦和温升修正,对比分析了摩擦-温度修正... 在变形温度为850~1100℃、应变速率为0.001~0.1 s^(-1)的条件下,利用Thermecmastor型热模拟试验机研究了锻态GH4706高温合金的热变形行为。综合考虑绝热温升和摩擦效应,对真应力-真应变曲线进行摩擦和温升修正,对比分析了摩擦-温度修正后的Arrhenius和Hansel-Spittel模型的相关系数r和平均相对误差AARE。结果表明:随着温度的降低和应变速率的提高,锻态GH4706高温合金的整体变形抗力逐渐变大,摩擦-温升效应所带来的误差也相对更大。建立的Arrhenius和Hansel-Spittel本构模型的相关系数分别为0.970和0.986,平均相对误差分别为13.17%和7.83%,Hansel-Spittel模型的预测精度更高。GH4706高温合金的动态再结晶对温度更为敏感,温度的升高有利于合金的动态再结晶,而应变速率的升高则会抑制合金的动态再结晶。 展开更多
关键词 GH4706高温合金 摩擦-温度修正 本构模型 热变形行为 动态再结晶
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