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CHE/ME 109 Heat Transfer in Electronics. LECTURE 19 – NATURAL CONVECTION FUNDAMENTALS . NATURAL CONVECTION MECHANISMS. NATURAL CONVECTION IS THE RESULT OF LOCALIZED DENSITY DIFFERENCES THESE CAN BE DUE TO DIFFERENCES IN COMPOSITIONS
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CHE/ME 109 Heat Transfer in Electronics LECTURE 19 – NATURAL CONVECTION FUNDAMENTALS
NATURAL CONVECTION MECHANISMS • NATURAL CONVECTION IS THE RESULT OF LOCALIZED DENSITY DIFFERENCES • THESE CAN BE DUE TO DIFFERENCES IN COMPOSITIONS • FOR HEAT TRANSFER THEY ARE GENERALLY RELATED TO TEMPERATURE DIFFERENCES • CONCENTRATION BASED CONVECTION INCLUDES CLOUD FORMATIONS • WATER HAS A LOWER MOLECULAR WEIGHT THAN AIR • CONCENTRATIONS OF WATER WILL TEND TO RISE THROUGH AIR DUE TO CONVECTION TO FORM CLOUDS • CUMULONIMBUS CLOUD FORMATION AS A RESULT OF CONVECTION. THE CLOUD TRACES THE PATH OF THE CONVECTION CURRENTS. http://blogs.sun.com/staso/resource/cumulonimbus-cloud-akbhhf-sw.jpg
CLOUD FORMATION H • THIS MECHANISM IS BASED ON NATURAL CONVECTION
CLOUD FORMATIONS • TEMPERATURE DIFFERENCES WILL ALSO RESULT IN ADVECTION, A HORIZONTAL TRANSFER OF HOT AIR OVER COLD AIR • NIMBOSTRATUS CLOUDS FORMED DUE TO ADVECTION. CLOUDS SHOW THE HORIZONTAL CURRENTS http://cimss.ssec.wisc.edu/satmet/modules/clouds/lowclouds2.html
SURFACE WINDS • THE RESULT OF PRESSURE DIFFERENCES. • THE FLOW OF COOL AIR FROM THE OCEAN TO THE COAST IS THE RESULT OF THIS TYPE OF NATURAL CONVECTION • THE MOST EXTREME EXAMPLES OF THESE FLOWS CAN RESULT IN THE FORMATION OF TORNADOES, CYCLONES AND HURRICANES http://www.berkeleycitycollege.edu/faculty/rhaberlin/images/pwppthl.gif
SEA AND LAND FLOWS • THESE ARE BASED ON DENSITY DIFFERENCES THAT RESULT IN PRESSURE VARIATIONS http://www.free-online-private-pilot-ground-school.com/images/sea-land-breeze.gif
DENSITY DIFFERENCES • DEFINED IN TERMS OF VOLUME EXPANSION COEFFICIENT • DERIVATION OF CHANGES IN DENSITY FOR FLUIDS: • VOLUME EXPANSIVITY: • ISOTHERMAL COMPRESSIBILITY:
DENSITY DIFFERENCES • FOR IDEAL GASES: • SO AROUND AMBIENT TEMPERATURE β = 3.3x10-3 K-1 = 1.8x10-3 R-1 • FOR LIQUIDS THE VALUES ARE ON THE ORDER OF β = 3x10-4 K
GRASHOF NUMBER • FLUID MOTION OCCURS DUE TO BOUYANCY EFFECTS AS PER (FIGURE 9-6) • ONCE THE FLUID IS IN MOTION, THEN VISCOUS EFFECTS OCCUR • COMPLETING A MOMENTUM BALANCE FOR A NATURAL CONVECTION FLOW WITH VELOCITIES IN THE x AND y DIRECTION (u AND v RESPECTIVELY) CONSIDERED YIELDS (9-13):
GRASHOF NUMBER • GRASHOF NUMBER IS THE RATIO OF THE BOUYANCY FORCES TO THE VISCOUS FORCES • VALUE OF THE GRASHOF NUMBER CAN BE LINKED TO FLOW REGIMES FOR NATURAL CONVECTION
NATURAL CONVECTION OVER SURFACES • FOR NATURAL CONVECTION HEAT TRANSFER PROCESSES • THE CORRELATIONS FOR HEAT TRANSFER COEFFICIENTS ARE BASED ON THE RAYLEIGH NUMBER: Ra = GrPr • Ra IS THE NATURAL CONVECTION EQUIVALENT OF THE PECLET NUMBER, Pe = RePr FOR FORCED CONVECTION
NATURAL CONVECTION OVER SPECIFIC SHAPES • VERTICAL FLAT PLATES • BOUNDARY LAYER STAYS AGAINST THE SURFACE AND THE FLOW REGIME CHANGES WITH DISTANCE. • TRANSITION TO TURBULENCE IS GENERALLY DEFINED IN TERMS OF THE Ra NUMBER AT Ra > 109. • EQUATIONS ARE DEVELOPED • FOR CONSTANT TEMPERATURE OR CONSTANT HEAT RATE • BASED ON FILM TEMPERATURE EQUAL TO (Ts - T )/2 • APPLY EQUALLY TO HOT OR COLD WALLS, RELATIVE TO T∞
NATURAL CONVECTION OVER SPECIFIC SHAPES • VERTICAL CYLINDERS CAN BE ANALYZED WITH THE VERTICAL PLATE EQUATIONS AS LONG AS THE DIAMETER IS LARGE ENOUGH
INCLINED PLATES AND FLAT PLATES • HAVE DIFFERENT FLOW PATTERNS FOR PLATE TEMPERATURES • GREATER THAN THE SURROUNDINGS • LOWER THAN THE SURROUNDINGS
INCLINED PLATES AND FLAT PLATES • HAVE DIFFERENT CORRELATIONS FOR TOPS OF PLATES AND BOTTOMS OF PLATES • )INCLINED PLATES CAN USE VERTICAL • PLATE CORRELATIONS BY REPLACING g IN THE Gr NUMBER WITH g(cos θ): • FOR THE TOP OF COOLED PLATES OR THE BOTTOM OF HEATED PLATES • FOR θ < 60 • FOR OTHER SITUATIONS, THE BOUNDARY LAYER BREAKS UP AND A SINGLE CORRELATION IS NOT PRACTICAL
HORIZONTAL PLATES • USE DIFFERENT CORRELATIONS BASED ON Lc = As/P FOR • THE UPPER SURFACE OF A HEATED PLATE OR THE LOWER SURFACE OF A COOLED PLATE (9-22 & 9-23) • THE LOWER SURFACE OF A HEATED PLATE OR THE UPPER SURFACE OF A COOLED PLATED (9-32)
HORIZONTAL CYLINDERS • THE BOUNDARY LAYER FORMS AROUND THE RADIUS AS SHOWN IN FIGURE 9-12 • SINGLE CORRELATION IS PROVIDED (9-25) APPLIES TO • LAMINAR CONDITIONS Ra < 1012 • FOR TURBULENT FLOW Ra > 109:
OTHER CORRELATIONS • FOR CONSTANT SURFACE TEMPERATURE , VALUES ARE BASED ON THE GENERAL FORMULATION: • SPHERES ARE MODELED USING (9-26) FROM IRVINE & HARTNETT (Eds), ADVANCES IN HEAT TRANSFER, Vol 11, 1975, Pp. 199-264