turbulent dispersion of aircraft exhausts in regions of breaking ...
turbulent dispersion of aircraft exhausts in regions of breaking ...
turbulent dispersion of aircraft exhausts in regions of breaking ...
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3108 A. DO RNBRACK and T. DU RBECK<br />
Fig. 2. Contours plots <strong>of</strong> the y-averaged temperature (left) and concentration fields (right) evolv<strong>in</strong>g <strong>in</strong> time.<br />
The three Gaussian plumes (cf. equation (2)) are emitted <strong>in</strong>stantaneously at t"71 m<strong>in</strong> (a) after model<br />
<strong>in</strong>itialization. The temporal <strong>in</strong>terval between the panel rows (a) to (d) is 13 m<strong>in</strong>. The thickness <strong>of</strong> the black<br />
temperature segments amounts to 0.007῀Θ. Broader (th<strong>in</strong>ner) segments <strong>in</strong>dicates reduced (enhanced)<br />
thermal stability. The contour levels <strong>of</strong> the concentration field are equidistant and are chosen uniformly for<br />
all plots.<br />
Fig. 3. As Fig. 2 for a plume released at t"116 m<strong>in</strong> after model <strong>in</strong>itialization. Aga<strong>in</strong>, the temporal <strong>in</strong>terval<br />
between the panel rows is 13 m<strong>in</strong>.