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 http://blogs.sun.com/staso/resource/cumulonimbus-cloud-akbhhf-sw.jpg THE PATH OF THE CONVECTION CURRENTS. 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-landbreeze.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