A SENSITIVE FAST-RESPONSE PROBE TO MEASURE TURBULENCE AND HEAT-FLUX FROM ANY AIRPLANE

被引:90
作者
CRAWFORD, TL
DOBOSY, RJ
机构
[1] National Oceanic and Atmospheric Administration, Air Resources Laboratory/ATDD, Oak Ridge, 37831, TN
关键词
D O I
10.1007/BF00119816
中图分类号
P4 [大气科学(气象学)];
学科分类号
0706 ; 070601 ;
摘要
The theory, configuration, and accuracy of an inexpensive probe to measure turbulence from a small airplane are presented. The probe employs a nine-hole pressure-sphere design along with inprobe high-frequency pressure, temperature, and acceleration sensors. This sensor suite is specifically designed to extend mass, momentum and energy eddy-flux measurement to the higher frequencies characteristic of marine and nocturnal boundary layers. The probe is part of a mobile flux system. independent of the conveyance, which does not require a separate Inertial Navigation System. The new nine-port pressure sphere turbulence probe allows accurate turbulent velocity measurement with proper probe installation and appropriate computation technique for dynamic pressure. A thermistor in the central pressure port provides simultaneous temperature measurement, at a location symmetrical with respect to the flow, for accurate determination of true airspeed and heat flux. The probe-amounted temperature sensor gives heat fluxes with variance 5% of the mean in a weakly-turbulent marine boundary layer.
引用
收藏
页码:257 / 278
页数:22
相关论文
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