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<br />. <br /> <br />. <br /> <br />3.8 <br /> <br />. <br /> <br />3.9 <br /> <br />. <br /> <br />3.10 <br /> <br />3.11 <br /> <br />. <br /> 3.12 <br />. <br /> 3.13 <br />. <br /> 3.14 <br /> <br />. <br /> <br />3.15 <br /> <br />. <br /> <br />4.1 <br /> <br />. <br /> <br />. <br /> <br />Same as Fig. 3.1, except of vertical (w') and true air- <br /> <br />spe~d (TAS') wind components. <br /> <br />Mean wind velocities of the Wyoming KIA versus the NCAR <br /> <br /> <br />Q/A of longitudinal (u), lateral (V), vertical (W) and <br /> <br /> <br />true airspeed (TAS) <br /> <br />. . . . . . . . . . .. . . <br /> <br />Same as Fig. 3.9, except for wind velocity variances. . . <br /> <br />Power spectra from the Wyoming KIA and NCAR Q/A of <br /> <br />longitud ina 1 (u'), latera 1 (v'), vert ica 1 (w') and true <br /> <br />aix;speed (TAS') . . . . . . . . . . . . . <br /> <br />The white noise test. Power spectral densities of two <br />I <br /> <br />diiferent random processes, coherence and phase func- <br />I <br /> <br />t ions are presented as a func t ion 0 f fre quenc ies. . . <br /> <br />Co~erence analysis between the Wyoming KIA and the NCAR <br /> <br />Q/~, of longitudinal (u'), lateral (v'), vertical (w') <br /> <br />and true airspeed (TAS'). . . . . . . . . . . . . <br /> <br />Phase shift analysis between the Wyoming KIA and the <br /> <br />NCAR Q/A, of longitudinal (u'), lateral (v'), vertical <br /> <br />(w') and true airspeed (TAS') . <br /> <br />Typical horizontal wind spectrum under negligible <br /> <br />tu~bulence conditions. <br /> <br />. . . . . . . . . . . . . <br /> <br />Au:tocorrelation functions from an aircraft [~(l)]' <br />E L <br />Eu.lerian [Ri(,)), and Lagrangian [Ri(,)] frame of refer- <br /> <br />ence (from Karacostas, 19(8). . . . . . . . . . . <br /> <br />vii <br /> <br />31 <br /> <br />32 <br /> <br />34 <br /> <br />35 <br /> <br />39 <br /> <br />40 <br /> <br />41 <br /> <br />44 <br /> <br />56 <br />