turbulent heating meaning in English
湍流加热
紊劣热
紊流加热
Examples
- The second mode shows a peak at 2 - 3 years . in equatorial cold tongue region , sst anomalies have great influence on the variation of turbulent heat fluxes . while out
在第二模态中，由sstdipole驱动的越赤道的异常风，只在sst梯度较大的北半球oon一10on的区域较强。 - The variation of sensible heat flux is dominated by air - sea temperature difference . interannual variability of turbulent heat fluxes is examined using svd , eof and mtm methods
热带太平洋enso事件通过对walker环流的调整减小热带大西洋itcz区的风速值，湍动热通量亦随之减小。 - The numerical analysis indicates that that the multi - longitudinal vortex flow in tubes can markedly enhance both the laminar and turbulent heat transfer with less additional increase of flow resistance
结果表明，管内多纵向涡对层流和湍流换热的强化效果显著而流阻增加较少，具有优良的综合强化换热性能。 - Abstract : approximate methods for calculating aerodynamic heating rates on space shuttles are discussed . various methods are given for predicting the heating rate at axisymmetric stagnation points , general three dimensional stagnationpoints and the leading edge stagnation point of wings . numerous laminar and turbulent heating techniques for flat plates and cones are analyzed and compared . a brief review of some methods is presented to predict heating rate for winward centerline and lateral direction off the symmetry plane . the results show that the methods are simpler and can guarantee enought precision for predicting aerodynamic heating environment of space shuttles
文摘:介绍了国内外预测航天飞机气动加热的工程计算方法.给出了轴对称、非轴对称和机翼前缘等各种外形驻点热流密度的计算，分析和比较了平板、锥体的层流和湍流热流密度计算的各种方法，概述了航天飞机迎风面中心线和离开中心线横向热流密度的计算.计算结果表明，本文方法用在航天飞机气动热环境初步设计中比较简单并且有足够精度 - It is found that two main eof modes of turbulent heat fluxes mainly describe the flux variations in two trade wind regions . the mtm spectrum of the first time series of expansion coefficient shows a periodic signal at about two - to - three months and two - to - three years quasi - periodic signal ( at the 95 % level )
热带大西洋的增暖事件中，东风减弱，西风加强，赤道冷舌区海洋的潜热和感热损失随sst的增暖而增大， itcz区海洋的潜热和感热损失则伴随着风速的减小而减小。