Laserfiche WebLink
<br />. <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br />t <br /> <br />is likely to be. The crosswind sampling line end points will be adjusted in accordance with <br />updated wind observations. <br /> <br />Airborne sampling may sometimes be unsafe when strong winds and turbulence are present, and <br />missions may be terminated at the pilot's discretion. The pilot-in-command always has ultimate <br />responsibility for maintaining aircraft and crew safety. <br /> <br />2.3.1 Field Preparation <br /> <br />Preparation for data collection effort will focus on preparation of the WMI transport and <br />dispersion model for the Santa Barbara terrain, selection of preferred site for the release of <br />rawinsondes, pre-project preparation and calibration of the SF6 detector, preparation of the <br />research aircraft itself, and the development of a detailed field operations plan. <br /> <br />Transport And Dispersion Modeling <br />The WMI transport and dispersion model follows the approach of the "GUIDE" model initially <br />developed under the auspices of the Bureau of Reclamation during Project Skywater. The first <br />use was for the Sierra Nevada Cooperative Pilot Project (SCPP) in the 1980's (Elliott 1981). <br />Subsequent development of the model occurred in 1984-1985 (Rauber et ai. 1988), and the first <br />applications were for aerially-released lines of AgI seeding agent. The model was intended to be <br />a simple operational application that could be run in near real-time. Since SCPP, other versions <br />of the model have been applied; e.g., testing of propane seeding in 1993-1994 (Reynolds 1996). <br />A GUIDE-type model was selected for development and application by WMI because it can be <br />run rapidly on a PC in the field, and configuration for specific target areas is straightforward. <br /> <br />GU \ 9 ~ <br />~ 1l1. <br /> <br />oJ- <br />w",1? <br /> <br />51) ~ <br /> <br />The flow over mountainous terrain is modeled by arbitrarily dividing the lower atmosphere into <br />several flow channels, or layers. The channels' vertical thicknesses are a function of elevation, <br />with higher terrain producing vertical constriction. At some level and above, there is no chimge <br />of channel thickness in response to terrain. In the examples presented herein, this level was <br />assumed to be 650 hPa. The mass flux perpendicular the barrier is assumed to be constant for <br />each channel. This produces an increased cross-barrier wind component over higher terrain. <br />The flow component parallel to the barrier is assumed to be unchanged. <br /> <br />Each grid point has a representative elevation. If Ui,j is the wind component parallel to the up- or <br />downslope direction at grid point i,j, then, <br /> <br />UiJ = Uc (APc)(LlPi,jyl , <br /> <br />(1) <br /> <br />where Uc is the mean wind for channel c, derived from a sounding, LlP c is the depth of the <br />initialized channels of the sounding, and LlPi,j is the depth of the channel at grid point i,j. <br />Equation (1) forces the flows within channels to meet the conservation of mass flux crite::1um <br />throughout the model grid. For all but the surface channel, LlP c has been set to 50 hPa. The <br />distance between adjacent grid points can be varied, but there are tradeoffs that effect model run <br />time, terrain smoothing, computer memory requirements, and resolution. Larger spa.cing <br />decreases run time, memory requirements, and resolution, and results in less detail in the terrain. <br />Smaller spacing increases run-time, memory requirements, and resolution, and allows more <br />Weather Damage Modification Program 31 <br />