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Last modified
7/28/2009 2:35:30 PM
Creation date
3/11/2008 2:42:50 PM
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Template:
Weather Modification
Title
Cloud Physics Studies in Utah During 1978
Date
9/1/1978
State
UT
Weather Modification - Doc Type
Report
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<br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />J <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br /> <br />CHAPTER 2 <br />DESCRIPTION OF INSTRUMENTED KING AIR AIRCRAFT <br /> <br />The Wyoming KIA has been described in detail by Cooper (1978). A <br />summary of its instrumentation is presented in Tables 2.1.1 and 2.1.2, and <br />an example of the images obtained by the 2D-probes is shown in Figure 2.1.1. <br />In addition to the instruments described by Cooper, we also had onboard an <br />NCAR ice nucleus counter. Data have been presented by Marwitz ~~. 1978 <br />showing that when the aircraft was flown through a sharp, distinct plume <br />of Agl, the NCAR counter would indicate the maximum concentration of ice <br />nuclei ~ 65 s later. Approximately 35 s after the observed peak in con- <br />centration, the NCAR counter would then indicate concentrations having a <br />value of 37% (e-1) of the peak concentration. <br />We experienced four equipment problems with the KIA during the field <br />project. During the first two flights on 12 March it was noted that the <br />indicated airspeed system malfunctioned during rapid descent. The aircraft <br />was flown back to Laramie and a permanent fix was made. No subsequent <br />problems were experienced with the indicated airspeed system. <br />During the project, the MRI turbulence system was determined to be <br />reading too high. The system was subsequently returned to the manufacturer <br />for repairs, and it was not available for the rest of the season. <br />The static pressure transducer produced a large number of spike-type <br />signals. These spikes permeated into a large number of other derived <br />parameters which are dependent on static pressure. The spikes are readily <br />evident in the analog traces. <br />Accurately measuring the liquid water content was the most difficult <br />problem. A Forward Scattering Spectrometer Probe (FSSP) and a Johnson- <br />Williams (JW) liquid water content Instrument were operated on the KIA. <br />We determined the liquid water content by integrating the FSSP spectra. <br />However, data obtained from these two sources consistently showed poor <br />agreement in that the liquid water contents obtained from the FSSP were <br />almost always higher than the liquid water contents measured by the JW <br />instrument. An example of the correlation between these instruments is <br />shown in Figure 2.1.2. This figure is a scatter diagram of FSSP water <br /> <br />3. <br />
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