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<br />504 <br /> <br />JOURNAL OF CLIMATE AND APPLIED METEOROLOGY <br /> <br />VOLUME 23 <br /> <br />estimates wherever. the null hypothesis was rejected, <br />is evident from the statement of the physical hypothesis <br />in Table 2. <br /> <br />6. C~)Oduct of the experiment <br /> <br />A partial simulation of the planned experiment was <br />carried out using data obtained on HIPLEX-I type <br />clouds during the preliminary field investigations, along <br />with estimates of probable seeding effects (Mielke et <br />al.. 1984). The results suggested that, for the three <br />response variables considered (CIC5, PIC8, TFPI), <br />about 50-150 test cases would be needed to reject the <br />null hypothesis. Section IV of the design document <br />(Bureau of Reclamation, 1979) estimated 30-45 test <br />case clouds per summer, so that an experiment of 2- <br />3 years duration was anticipated. Regrettably, nature <br />failed to match the climatological estimate and so a <br />longer experiment was needed. It IS equally regrettable <br />that budgetary mandates terminated the experiment <br />before it could be extended beyond two years. <br />The HIPLEX-l experiment began in the summer <br />of 1979 and continued through the summer of 1980. <br />An initial start was made early in 1979, but it quickly <br />became evident that the experimental procedures were <br />not completely satisfactory. The use of the HIPLEX <br />Z-R relationship for subcloud regions that contained <br />substantial amounts of precipitating ice particles was <br />regarded as questionable. Therefore a provision was <br />added to constrain the RERC calculation to cases where <br />the center of the radar beam at the lowest tilt angle <br />(0.70) was at or below the + WOC level; the presence <br />of any ice particles would then be less likely to affect <br />the calculation. ~ome details of the flight procedures <br />were clarified; some computational procedures related <br />to where average values were to be taken were changed; <br />and some provisions further specifying default values <br />were added. Perhaps the most important lesson from <br />this experience was that, before launching such an ex- <br />periment, at least one trial case should be completed <br />and run all the way through the data reduction process <br />in order to uncover any unsuspected deficiencies in <br />the procedures. . <br />After the procedures were modified, the experiment <br />was restarted and 12 test cases were recorded during <br />the latter half of the summer. The summer of 1980 <br />was extremely dry in eastern Montana and only eight <br />additional test cases were logged that year. Especially <br />in 1980, the measured liquid water concentrations of <br />many of the candidate clouds were not sufficient to <br />meet the selection criteria. Numerous additional clouds <br />not meeting these criteria were also studied each sum- . <br />mer, but not as part of the randomized seeding ex- <br />periment. HIPLEX-I was pre-empted by the Coop- <br />erative Convective Precipitation Experiment (CCOPE) <br />in 1981, and then terminated. As a result, only 20 <br />total cases are available for analysis, with seven clouds <br />being assigned to Class A-I and 13 to Class B. <br /> <br />a. Experimental procedures <br /> <br />The HIPLEX-I experiment was carried out within <br />the framework of a general operations plan covering <br />all aspects from forecasting to debriefing of the missions <br />(see Appendix C of Bureau of Reclamation, 1979). In <br />the conduct of HIP LEX-I, the key elements were thl~ <br />seeding aircraft, the cloud physics aircraft, and thl~ <br />SWR-75 radar. The seeding aircraft was a Lea1jet, whik <br />the cloud physics aircraft was a King Air. Appendix <br />G of the design document (Bureau of Reclamation, <br />1979) describes the operating capabilities and instru.. <br />mentation of the aircraft. All of the instrumentation <br />was calibrated according to the normal procedures; in <br />addition, the aircraft instrumentation was calibrated <br />during tower fly-bys and checked in comparison flights <br />involving other project aircraft. <br />Detailed operational procedures were spelled out <br />for the aircraft (see Section VIII of Bureau of Recla-. <br />mation, 1979). In brief, the seeding aircraft determined <br />the cloud top temperatures and rate of growth, and <br />conducted the treatment runs at or near the cloud tops <br />(Fig. 2). The cloud physics aircraft made an initial <br />pretreatment pass through each candidate cloud to <br />determine whether it met the selection criteria (see <br />Section 3). If it did, the cloud was treated and the <br />cloud physics aircraft then made a series of passes <br />through it to look for the development of ice crystals <br />and the initial precipitation particles. <br />The first two post-treatment passes were targeted <br />for 0.3 km below treatment altitude, or usually around <br />the -80C level, at about 2 ~in and 5 min after treat- <br />ment, respectively. (The treatment time was taken as <br />30 s after activation of the selected dry-ice dispenser, <br />to allow time for the pellets to reach the intended <br />region of the cloud.) They were made in a direction <br />perpendicular to the treatment pass (Fig. 3) in an at- <br />tempt to intersect the seeded curtain. Subsequent passes <br />at about 8, II, 14, and 17 min after treatment (or <br />until an echo appeared on the aircraft 3-cm weather <br />radar) were targeted for the -50C level (Fig. 4). Mean- <br />while, the seeding aircraft continued to monitor the <br />cloud top for 10 min after treatment, to observe any <br />changes in its height or temperature. It also collected <br />data on ice crystals in the top of the cloud, for the <br />physical evaluation, when the cloud top remained <br />above the aircraft's lowest allowable flight level. <br />The cloud physics aircraft then descended to the <br />+ WOC level to monitor the precipitation falling from <br />the cloud. It made a series of orthogonal passes, at <br />about 3-min intervals, through the rain shaft. Mean-. <br />while the SWR-75 radar conducted a continuous series <br />of 3-min volume scans beginning at an elevation angle <br />of 0.70. The next elevation step was 1.00, and sub- <br />sequent increments were 10 for nearby test cases and <br />0.50 for cases beyond about 80 km range. Observations <br />continued until the termination of the test case, 40 <br />min after treatment. Close time lines were specified <br />