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transition from laminar to turbulent flow and also represents a point of <br /> diminishing returns Beyond this point, even significant increases in vacuum <br /> tend to yield only minor increases in flow <br /> Once the optimum extraction flow rate has been established,the SVE pilot <br /> test will be conducted to establish the relationship between distance from the <br /> extraction well and vacuum in the vadose zone This relationship will then be <br /> used to estimate the effective radius of influence corresponding to the selected <br /> flow rate and well construction Radius of influence is typically estimated by <br /> interpolating the distance from the extraction well, which corresponds to a <br /> minimum vacuum of 0 05 inches of water This interpretation can be <br /> iperformed graphically on a semi-log plot of vacuum vs distance <br /> To establish the relationship between vacuum and distance, soil vapors will be <br /> extracted at a fixed flow rate and vacuum from the SVE well Following <br /> stabilization of soil vapor flow conditions, vacuum readings will be recorded <br /> for several existing vadose zone monitoring points located at known distances <br /> from the SVE well Stabilization will be evaluated by frequently monitoring <br /> vacuum readings at the monitoring points When vacuum readings have <br /> remained essentially constant for at least one hour, conditions will be <br /> considered stable <br /> Two soil vapor samples will also be collected for laboratory analysis of BTEX <br /> and total petroleum hydrocarbons TPH, by USEPA Method TO14 One <br /> sample will be collected approximately 30 minutes after startup and another at <br /> the conclusion of the SVE pilot testing activities Results of the laboratory <br /> analyses will be used to calculate projected removal rates, carbon usage, and <br /> air emissions based on the design flow rate of the full-scale system Potential <br /> breakthrough of contaminant air emissions will be monitored using a <br /> photoionization detector(PID) at points immediately downstream of each <br /> carbon vessel <br /> 3.3 Combined AS/SVE Pilot Test <br /> After stabilization of SVE flow, the SVE blower will remain in operation <br /> while a brief step-AS test is performed to establish sparging breakout pressure <br /> and optimum sparging flow rate The AS testing will be conducted on - <br /> existing well SP-1 This well is constructed of 48 feet of blank '/4-inch <br /> diameter PVC material attached to a 2 feet long ceramic air diffuser <br /> Construction of SP-1 is detailed in the Figures section <br /> The step-AS test will involve injecting air into SP-1 at several different <br /> injection pressures while observing the corresponding flow rates As injection <br /> pressures are increased, a point will be reached at which flow is initiated <br /> This injection pressure is defined as the breakout pressure and should <br /> ii <br /> Pilot Testing Work Plan <br /> 1717 South Center Street-Stockton,California <br /> Prepared by Philip Services Corp <br /> H 5EN 24001321121382EG1Pmj3 ctsLSrockCenllp$loite tplm doc July 23,2002 <br />