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Methodology for the Evaluation of Natural Ventilation in ... - Cham

Methodology for the Evaluation of Natural Ventilation in ... - Cham

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The average and exhaust <strong>in</strong>ternal build<strong>in</strong>g temperatures were known <strong>for</strong> both <strong>the</strong> prototypebuild<strong>in</strong>g and <strong>the</strong> reduced-scale air model. The ambient temperature was known <strong>for</strong> each case aswell. The height <strong>in</strong> <strong>the</strong> buoyancy <strong>for</strong>ce calculation used was <strong>the</strong> overall build<strong>in</strong>g/model height,15m <strong>for</strong> <strong>the</strong> build<strong>in</strong>g and 1.2 meters <strong>for</strong> <strong>the</strong> model.In <strong>the</strong> prototype build<strong>in</strong>g field measurements, <strong>the</strong> air velocity <strong>for</strong> <strong>the</strong> surround<strong>in</strong>g environmentwas known from recorded data at <strong>the</strong> wea<strong>the</strong>r station. The enter<strong>in</strong>g air velocity at <strong>the</strong> awn<strong>in</strong>gtypew<strong>in</strong>dow was known <strong>for</strong> several site visits, and was measured <strong>in</strong> <strong>the</strong> horizontal plane <strong>of</strong> <strong>the</strong>w<strong>in</strong>dow (neglect<strong>in</strong>g <strong>the</strong> side/vertical pieces and <strong>the</strong>ir contribution). For <strong>the</strong> reduced-scale airmodel, <strong>the</strong> enter<strong>in</strong>g air velocity was known at <strong>the</strong> w<strong>in</strong>dow face, which was a vertical, rectangularopen<strong>in</strong>g <strong>in</strong> <strong>the</strong> façade. S<strong>in</strong>ce <strong>the</strong> velocities were at different locations and <strong>for</strong> different w<strong>in</strong>dowconfigurations, <strong>the</strong> pressures due to w<strong>in</strong>d and buoyancy were used ra<strong>the</strong>r than <strong>the</strong> buoyant andreference velocities. The Archimedes number <strong>the</strong>n could be calculated as:PBAr (7.7)PWFrom Chapter 2, <strong>the</strong> pressure due to buoyancy, or <strong>the</strong> stack effect, was given as: TI TOP BOgH(7.8) TIThe pressure due to w<strong>in</strong>d was given as:2U POw CPO(7.9)2with C p equal to <strong>the</strong> (C p upw<strong>in</strong>d -C p downw<strong>in</strong>d ) The pressure due to w<strong>in</strong>d could also be calculated us<strong>in</strong>g<strong>the</strong> power law equation:PQ cdA 2 (7.10)The pressure difference could be calculated based on <strong>the</strong> flow rate through <strong>the</strong> model. After this,re-arrang<strong>in</strong>g, equation 7.10 becomes:2 Q 1 PW A2 (7.11)Cd Where Q is <strong>the</strong> flow rate, A is <strong>the</strong> area <strong>of</strong> <strong>the</strong> <strong>in</strong>let open<strong>in</strong>g, and C d is <strong>the</strong> discharge coefficient,normally estimated as 0.6 <strong>for</strong> w<strong>in</strong>dows.7.3 Measurements and Results <strong>for</strong> <strong>the</strong> Prototype Build<strong>in</strong>gThe goal <strong>of</strong> <strong>the</strong> reduced-scale air model is to predict <strong>the</strong> ventilation per<strong>for</strong>mance <strong>of</strong> a full-scalebuild<strong>in</strong>g, us<strong>in</strong>g temperature distributions and airflow patterns. Data from <strong>the</strong> reduced-scale airmodel, reduced-scale CFD model, and full-scale CFD model were compared to <strong>the</strong> prototypebuild<strong>in</strong>g. The models predicted steady-state conditions <strong>for</strong> a given ambient temperature and<strong>in</strong>ternal load, while <strong>the</strong> prototype build<strong>in</strong>g was operat<strong>in</strong>g under transient conditions. Thereduced-scale model was created based on a typical temperature differential between <strong>in</strong>terior andexterior temperature <strong>of</strong> 5-8°C.150

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