Solar Constant Emissivity Albedo

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Presentation transcript:

Solar Constant Emissivity Albedo

Topic 8: Energy production 8.2 – Thermal energy transfer The solar constant PRACTICE: The sun radiates energy at a rate of 3.901026 W. What is the rate at which energy from the sun reaches Earth if our orbital radius is 1.51011 m? SOLUTION: ASPHERE = 4r2. Recall that intensity is the rate at which energy is being gained per unit area. Then I = P / [ 4r2 ] = 3.901026 / [ 4(1.51011)2 ] = 1380 W m-2. This value is called the solar constant. intensity = power / A intensity © 2006 By Timothy K. Lund Psun = 1380 W m-2 the solar constant

Topic 8: Energy production 8.2 – Thermal energy transfer The solar constant PRACTICE: Explain why the solar intensity is different for different latitudes. SOLUTION: The following diagram shows how the same intensity is spread out over more area the higher the latitude. © 2006 By Timothy K. Lund 1380 W/m2 3

Topic 8: Energy production 8.2 – Thermal energy transfer The solar constant PRACTICE: The sun radiates energy at a rate of 3.901026 W. What is the rate at which energy from the sun reaches Jupiter if its orbital radius is 7.81011 m? (This is Jupiter’s solar constant.) SOLUTION: Use I = P / [ 4r2 ] I = P / [ 4r2 ] = 3.901026 / [ 4(7.81011)2 ] I = 51 W m-2. This is 51 J / s per m2. © 2006 By Timothy K. Lund

Topic 8: Energy production 8.2 – Thermal energy transfer Emissivity The emissivity e of a body is a number between 0 and 1 that quantifies the emission and absorption properties of that body as compared to a blackbody of equal size. A black-body is a perfect emitter / absorber of radiation and has an emissivity of e = 1. A body that can’t emit / absorb radiation at all has an emissivity of e = 0. The emissivity of a body is the ratio of the power emitted by the body, to the power emitted by a black-body of the same size. charcoal e = 0.95 mirror e = 0.05 © 2006 By Timothy K. Lund e = PBODY / PBLACK-BODY emissivity e = PBODY / [ AT 4 ]

Topic 8: Energy production 8.2 – Thermal energy transfer Emissivity A black-body is a perfect emitter/absorber (e = 1). A small sphere covered with lamp black makes a pretty good black-body and has an emissivity somewhat close to 1. An even better black- body is the metal- cavity black-body: If we know e, the Stefan-Boltzmann law can be amended: e = 0.9 e = 0.5 better black-body tallow candle © 2006 By Timothy K. Lund incident thermal radiation P = eAT 4 the Stefan-Boltzmann law where  = 5.6710-8 W m-2 K-4.

Topic 8: Energy production 8.2 – Thermal energy transfer PINCIDENT Albedo When light strikes an object, some of it is absorbed, and some of it is scattered. If light strikes a mirror, nearly all of it will be scattered: If light strikes a surface covered with lamp black, nearly all of it will be absorbed: We define albedo in terms of scattered and incident power: PSCATTERED heat PSCATTERED PINCIDENT © 2006 By Timothy K. Lund heat albedo = PSCATTERED / PINCIDENT albedo FYI The mirror has an albedo of almost 1. The black-body has an albedo of almost 0. 7

Topic 8: Energy production 8.2 – Thermal energy transfer Albedo Landforms, vegetation, weather, and seasons affect a planet’s albedo. The table shows that different terrains have different albedos. Ocean water scatters little light (7%). Snow and ice scatter a lot of light (62% to 66%). Desert (36%). © 2006 By Timothy K. Lund 8

Topic 8: Energy production 8.2 – Thermal energy transfer Albedo EXAMPLE: Satellites are used to map out monthly albedos. © 2006 By Timothy K. Lund White and gray areas: No data. Albedo April, 2002, Terra satellite, NASA 9

Topic 8: Energy production 8.2 – Thermal energy transfer Albedo From the previous table and satellite map it is clear that calculating the overall albedo of a planet is quite complex. Clouds (and even contrails) also contribute to the albedo. Overall, Earth’s mean yearly albedo is about 0.3 (or 30%). The actual albedo depends on season, latitude, cloud cover, and snow cover. It varies daily! © 2006 By Timothy K. Lund 10

Topic 8: Energy production 8.2 – Thermal energy transfer Solving problems involving albedo EXAMPLE: Assuming an albedo of 0.30, find, for Earth: (a) the power of the sunlight received. SOLUTION: Use I = 1380 W m-2 and I = P / A. The radius of Earth is r = 6.37106 m so its cross-sectional area is A = r2 = (6.37106)2 = 1.271014 m2. An albedo of 0.30 means that 70% of the sunlight is absorbed (because 30% is scattered). Thus P =(0.70)IA =(0.70)(1380)(1.271014) = 1.231017 W. Thus Earth intercepts energy from the sun at a rate of 1.231017 W. © 2006 By Timothy K. Lund

Topic 8: Energy production 8.2 – Thermal energy transfer Solving problems involving albedo EXAMPLE: Assuming an albedo of 0.30, find, for Earth: (b) the predicted temperature due to the sunlight reaching it. SOLUTION: From the previous example P = 1.231017 W. But this power is distributed over the whole rotating planet, which has an area Asphere = 4r2. From Stefan-Boltzmann we have P = AT4 1.231017 = (5.6710-8)4(6.37106)2T4 T = 255 K (-18°C). © 2006 By Timothy K. Lund

Topic 8: Energy production 8.2 – Thermal energy transfer Solving problems involving emissivity and Earth’s average temperature EXAMPLE: If the average temperature of Earth is 289 K, find its emissivity. SOLUTION: We determined that Earth absorbs energy from the sun at a rate of P = 1.231017 W. Since the temperature of Earth is relatively constant, we can assume it is radiating power at the same rate of PBODY = 1.231017 W. At 289 K the power radiated by a black-body of the same size as Earth is: PB-B = (5.6710-8)4(6.37106)22894 = 2.021017 W. Thus e = PBODY / PBLACK-BODY = 1.23 / 2.02 = 0.61. © 2006 By Timothy K. Lund

Topic 8: Energy production 8.2 – Thermal energy transfer Solving problems involving albedo albedo = PSCATTERED / PINCIDENT PINCIDENT = 340 W m-2 PSCATTERED = 100 W m-2 albedo = 100 / 340 © 2006 By Timothy K. Lund 14

the Stefan-Boltzmann law Solar Constant: Emissivity: Amended Stefan-Boltzmann Constant: Albedo: Psun = 1380 W m-2 the solar constant e = PBODY / PBLACK-BODY emissivity e = PBODY / [ AT 4 ] P = eAT 4 the Stefan-Boltzmann law where  = 5.6710-8 W m-2 K-4. albedo = PSCATTERED / PINCIDENT albedo