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Last modified
7/28/2009 2:40:01 PM
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4/23/2008 1:56:18 PM
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Weather Modification
Title
Dynamical and Microphysical Characteristics of Winter Storms over the Sierra Nevada
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<br />i 'i <br /> <br />DYNAMICAL AND MICROPHYSICAL CHARACTERISTICS <br /> <br />OF WINTER STORMS OVER THE SIERRA NEVADAS <br /> <br />John D. Marwitz and Ronald E. Stewart <br /> <br />University of Wyoming <br />La!amie, Wyoming <br /> <br />James A. ~10ore <br /> <br />U. S. Bureau of Reclamation <br /> <br />1. <br /> <br />INTRODUCTION <br /> <br />The Department of Atmospheric Science <br />at the University of Wyoming participated in the <br />1977-78 Sierra Cooperative Pilot Project (SCPP). <br />The Wyoming participation was with their newly <br />instrumented Beechcraft King Air cloud physics <br />aircraft. Two objectives were pursued by the <br />Wyoming group. They were to study the natural <br />dynamical and microphysical characteristics of <br />Sierra Nevada storms and to conduct transport and <br />diffusion (T&D) experiments which closely simula- <br />ted T&D during actual storm situations. In this <br />paper we will only discuss some preliminary re- <br />sults from the first objective. <br /> <br />The SCPP had a number of components <br />among which were the cloud physics aircraft oper- <br />ated by Wyoming, a.S-cm radar and rawinsonde <br />operated by North American Weather Consultants, <br />two 3-cm Doppler radars operated by NOAA/WPL, a <br />S-cm Doppler radar operated by NCAR, a tracer/ <br />seeder aircraft operated by Aero Systems, Inc. <br />and surface microphysics, precipitation and over- <br />all project direction by the Bureau of Reclama- <br />tion. Even though the tri-Doppler system and <br />tracer/seeder aircraft were not present in Dec:- <br />ember, it was considered worthwhile to describe <br />some preliminary results in this and other papers. <br />We mutually considered the storm of 14-15 Decem- <br />ber 1977 to be reasonably typical and the best <br />documented of those studied in December 1977. <br /> <br />2. <br /> <br />THE KING AIR DATA SYSTEM <br /> <br />The newly instrumented cloud physics <br />research aircraft is a Beechcraft Super 200 King <br />Air. This was the first field project in which <br />it was used. As such there were a number of <br />early failures of aircraft and data system com- <br />ponets plus a continual process of training new <br />crew members as well as developing procedures and <br />flight plans which would maximize the research <br />efforts. <br /> <br />To study the orographic storms it <br />was desirable to fly as close to the mountain <br />parrier as legal, and safety requirements would <br /> <br />.d <br />~ ,.: <br /> <br />allow. Since the aircraft was equipped with a <br />flight director system i.n which up to ten way- <br />points could be inserted, and flown in any de- <br />sired sequence, a letter of agreement Wa$ devQl- <br />oped among Oakland ARTCC, The Bureau of Reclama- <br />tion and the Department of Atmospheric Science. <br />The letter of agreement allowed Wyoming to fly <br />minimum obstruction clearance altitudes (MOCA) if <br />they accepted responsibility for mainta:1.ning their <br />own clearance of 2000 ft above and 5 NMi fro~ all <br />obstructions along their proposed flight path. <br />With this agreement and the assistance of the var- <br />ious FAA controllers, we were never restricted in <br />flying the research missions as desired. <br /> <br />The position keeping of t.he aircraft <br />was maintained by recording DME/vOR as well a. <br />heading, static pressure, indicated airspeed and <br />rate of climb. The horizontal winds were obtain- <br />ed with a Doppler navigation system Bind a deiced <br />yaw angle sensor located on a nose boom. The <br />vertical velocities were obtained witl. a vertical <br />accelerometer, pitch and roll gyros plus a deiced <br />angle of attack sensor also located on the nOS8 <br />boom. Two temperature probes were rE~corded: a <br />reverse flow and a Rosemount probe. The moisture <br />sensor was a dewpoint hygrometer. The cloud phy- <br />sics instruments consisted of four Particle Mea- <br />surement Systems probes which covered the range <br />of particles from I to 4500 pm. Two of the ima- <br />ging probes were 2-D probes. In addition, a J-W <br />liquid water content sensor, an MRI turbulence <br />sensor, an NCAR ice nucleus detector, a rotating <br />filter sampler for ice nuclei and a decelerator <br />for collecting ice crystals were also included. <br /> <br />To optimize the research missions the <br />scientist-copilot and scientist-data system oper- <br />ator could independently select any Ii of approxi- <br />mately 200 voltages, counts or derived parameters <br />for real time digital display. In addition the <br />scientists could view on a storage scope histo- <br />grams from the l-D PMS probes or images from the <br />2-D PMS probes. To further.optimize research <br />missions, to maintain data quality control and to <br />justify placing a number of scientists in the <br /> <br />149 <br /> <br />
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