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<br />45 <br /> <br />I <br /> <br />The crux of the problem in applying Taylor's theory is, therefore, to <br /> <br />I <br /> <br />determine the Lagrangian autocorrelation function. The Eulerian autocorrela- <br /> <br />tion function, R~, is rather more easily determined using instrumented towers <br />1 . <br /> <br />I <br />I <br /> <br />and instrumented aircraft flying through "frozen turbulence fields". <br /> <br />Eulerian autocorrelation data have been shown to fit a decaying exponen- <br /> <br />I <br />I <br /> <br />tial function both in the atmosphere and in wind tunnels (Comte-Bellot and <br /> <br />Corrisin, 1971). That is: <br /> <br />RE (T) ~ e-T/TE <br />i <br /> <br />(3.4) <br /> <br />I <br /> <br />where TE is the Eulerian characteristic time. <br /> <br />In the particular experiment, the characteristic time of the turbulence <br /> <br />I <br /> <br />as observed by the NCAR aircraft (TA) was determined in a manner to be <br /> <br />described later. The relation between TE and TA is: <br /> <br />I <br /> <br />GS <br />TE := TA lV'S <br /> <br />I <br /> <br />(3.5) <br /> <br />where GS is ground speed of the aircraft and WS is the wind speed. <br /> <br />I <br /> <br />By assuming similarity as suggested by Hay and pasquill (1959), we can <br /> <br />II <br /> <br />write: <br /> <br />R~ (T) <br />1 <br /> <br />e-T/TL ~ e-T/STE ~ e-T WS/STA GS <br /> <br />(3.6) <br /> <br />I <br />I <br /> <br />Fig. 3.6 is schematic of the three autocorrelation functions presented in <br /> <br />Equation 3.4, 3.5 and 3.6. <br /> <br />I <br /> <br />I <br /> <br />I <br /> <br />I <br />I <br />