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RADIATION AND COMBUSTION PHENOMENA
PROF. SEUNG WOOK BAEK DEPARTMENT OF AEROSPACE ENGINEERING, KAIST, IN KOREA ROOM: Building N7-2 #3304 TELEPHONE : 3714 Cellphone : 010 – TA : Jonghan Won ROOM: Building N7-2 # 3315 TELEPHONE : 3754 Cellphone :
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RADIATIVE HEAT TRANSFER
RADIATIVE EQUILIBRIUM INCIDENT RADIATION G R : ABSORPTIVITY T A : REFLECTIVITY : TRANSMISSIVITY OPAQUE SURFACE TRANSPARENT SURFACE PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE EQUILIBRIUM FOR AN OPAQUE SURFACE REFLECTION MODELS PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE EQUILIBRIUM HEAT FLUX FOR OPAQUE SURFACE G B E : RADIOSITY (NO RELATION TO MAGNETIC FIELD) : IRRADIATION OPAQUE PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE EQUILIBRIUM AN OPAQUE BODY IN AN INSULATED ENCLOSURE UNDER EQUILIBRIUM, THE FIRST LAW YIELDS , OR PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE EQUILIBRIUM By Definition : Emissivity is a measure of how well a body can radiate energy as compared to a blackbody Under Equilibrium : Kirchhoff’s Law PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE EQUILIBRIUM ALSO ELIMINATE , OR UNDER EQUILIBRIUM (OR ADIABATIC) PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
PART II. RADIATIVE NON-EQUILIBRIUM ENCLOSURE RADIATION PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM EXAMPLE APPLICATION TO THERMOS BOTTLE ANY EFFECT OF CONVECTION? EQUIVALENT CONDUCTION INSULATION thick cork is needed!!! PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM OPTICAL APPROACH IS HOPELESS FOR ENCLOSURES INVOLVING MORE THAN THREE SURFACES NEED ANOTHER APPROACH !!! TWO METHODS… ELECTRICAL ANALOGY NET RADIATION METHOD PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM ELECTRICAL ANALOGY (RADIATION NETWORK METHOD) TWO CIRCUIT ELEMENTS (RESISTANCES) SURFACE (COLOR) VOLUME (VIEW) SURFACE ELEMENT PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM 2. VOLUME ELEMENT FOR ENERGY LEAVING A SURFACE IF I IS ISOTROPIC PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM VIEW FACTOR A FRACTION OF TOTAL ENERGY LEAVING SURFACE INTERCEPTED BY SURFACE ENERGY FROM ENERGY FROM TO PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM BY DEFINITION HERE WITH PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM SIMILARLY WHICH LEADS TO THE RECIPROCITY RELATION CONSEQUENTLY, THE RECIPROCITY RELATION BETWEEN AND PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM BETWEEN AND AND BETWEEN AND FOR AN ENCLOSURE PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM NOW, BACK TO THE VOLUME ELEMENT!!! CONSIDER TWO SURFACES, SAY AND , OF AN ENCLOSURE RADIATION FROM TO RADIATION FROM TO PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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RADIATIVE HEAT TRANSFER
RADIATIVE NON-EQUILIBRIUM NET RADIATION (HEAT FLUX) BETWEEN AND BY RECIPROCITY THEN OR PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER
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