Methodology for the Evaluation of Natural Ventilation in ... - Cham
Methodology for the Evaluation of Natural Ventilation in ... - Cham
Methodology for the Evaluation of Natural Ventilation in ... - Cham
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Table 19. Summary <strong>of</strong> Values and Dimensionless Parameters <strong>for</strong> Full-Scale Build<strong>in</strong>g, Scaled Airand Scaled Water ModelsAir-Build<strong>in</strong>g Air-Model Water Model Water ModelScale 1 12 12 100g (m/s 2 ) 9.8 9.8 9.8 9.8β (1/°K) 0.0033 0.0034 0.0002 0.0002ΔT (°K) 5 30 6 6g'=gβΔT 0.1655 0.9800 0.0118 0.0118H=height <strong>of</strong> Atrium (m) 15 1.2 1.2 0.75α (m 2 /s) 2.16x10 -5 2.40 x10 -5 1.44 x10 -7 1.44x10 -7ν (m 2 /s) 1.477 x10 -5 1.60 x10 -5 1.01 x10 -6 1.01 x10 -6A CS (m 2 ) 6.32 0.522 0.559 0.037Pr 0.7 0.7 7.0 7.0Re 6.74x10 5 3.54 x10 4 1.10 x10 4 1.70 x10 4Pe=PrRe 4.72 x10 5 2.47 x10 4 7.68 x10 4 1.19 x10 5Gr 3.84 x10 13 7.94 x10 9 2.05 x10 8 3.65 x10 9Ra=PrGr 2.69 x10 13 5.56 x10 9 1.43 x10 9 2.55 x10 10For <strong>the</strong> reduced scale air model, <strong>the</strong> primary characteristic length used <strong>in</strong> evaluat<strong>in</strong>g <strong>the</strong> occupiedzones is <strong>the</strong> hydraulic diameter <strong>of</strong> <strong>the</strong> cross section <strong>of</strong> a s<strong>in</strong>gle floor. This parameter accuratelydescribes <strong>the</strong> ma<strong>in</strong> flow through <strong>the</strong> model and provides a characteristic length <strong>of</strong> 0.52m.However, <strong>the</strong> height <strong>of</strong> <strong>the</strong> atrium is used <strong>in</strong> evaluat<strong>in</strong>g <strong>the</strong> buoyancy velocity, s<strong>in</strong>ce it is <strong>the</strong>height difference between <strong>the</strong> <strong>in</strong>let and <strong>the</strong> outlet, at <strong>the</strong> top <strong>of</strong> <strong>the</strong> stack, which drives <strong>the</strong> airflow. The Reynolds number <strong>for</strong> <strong>the</strong> model was approximately 3.54x10 4 , us<strong>in</strong>g <strong>the</strong> hydraulicdiameter <strong>of</strong> a s<strong>in</strong>gle heated zone. This falls <strong>in</strong> <strong>the</strong> turbulent regime. The Grash<strong>of</strong> number <strong>for</strong> <strong>the</strong>scale model is on <strong>the</strong> order <strong>of</strong> 1.2x10 8 . When compar<strong>in</strong>g both <strong>the</strong> Reynolds number and Grash<strong>of</strong>number to those calculated <strong>for</strong> <strong>the</strong> prototype build<strong>in</strong>g <strong>for</strong> buoyancy-driven flow, <strong>the</strong> prototypebuild<strong>in</strong>g is also <strong>in</strong> <strong>the</strong> turbulent regime (Re=7.1x10 5 ) and buoyancy dom<strong>in</strong>ated flow(Gr=9.1x10 10 ). F<strong>in</strong>ally, <strong>for</strong> <strong>the</strong>rmal similarity <strong>the</strong> temperature differences and heat flow mustrema<strong>in</strong> proportional. The <strong>in</strong>ternal heat load per square meter (W/m 2 ) is scaled us<strong>in</strong>g <strong>the</strong> same12 th scale to provide <strong>the</strong> similar buoyancy effect. The temperatures recorded from <strong>the</strong> reducedscaleair model are non-dimensionalized us<strong>in</strong>g <strong>the</strong> ΔT ref to obta<strong>in</strong> <strong>the</strong> result<strong>in</strong>g full-scale build<strong>in</strong>gtemperatures <strong>for</strong> analysis.From Table 19, <strong>the</strong> critical Reynolds number, 2.3x10 3 is achieved <strong>for</strong> all models and <strong>the</strong> fullscaleprototype build<strong>in</strong>g. The air model achieves a slightly closer value <strong>of</strong> Reynolds number thanei<strong>the</strong>r <strong>of</strong> <strong>the</strong> water models, but is still <strong>of</strong>f by a factor <strong>of</strong> 10. When <strong>the</strong> Prandtl number isaccounted <strong>for</strong> us<strong>in</strong>g <strong>the</strong> Peclet number, Pe, <strong>the</strong> small-scale water model achieves a closer matchto <strong>the</strong> full-scale prototype than ei<strong>the</strong>r <strong>of</strong> <strong>the</strong> o<strong>the</strong>r models. It is assumed that each <strong>of</strong> <strong>the</strong> models,as well as <strong>the</strong> prototype build<strong>in</strong>g, is operat<strong>in</strong>g <strong>in</strong> a turbulent regime <strong>for</strong> <strong>the</strong> airflow <strong>in</strong> <strong>the</strong> heatedzone. For <strong>the</strong> buoyancy-driven case, equality <strong>of</strong> Grash<strong>of</strong> number is required after meet<strong>in</strong>g <strong>the</strong>critical Reynolds number condition. The twelfth-scale air model and 100 th scale water modelmore closely match <strong>the</strong> Grash<strong>of</strong> number, but none <strong>of</strong> <strong>the</strong> models matches it exactly. Someresearch (E<strong>the</strong>ridge and Sandberg 1996) that <strong>in</strong>dicates that <strong>for</strong> buoyancy-driven flow it issufficient to achieve critical values <strong>of</strong> Grash<strong>of</strong> number when us<strong>in</strong>g air as <strong>the</strong> work<strong>in</strong>g fluid.They propose a critical value <strong>of</strong> Grash<strong>of</strong> number <strong>in</strong> <strong>the</strong> range <strong>of</strong> 10 6 to 10 9 based on someexperimental work, and us<strong>in</strong>g <strong>the</strong> height <strong>of</strong> a room as <strong>the</strong> characteristic length. When <strong>the</strong> room90