## Approximate predictions of the transport of thermal radiation through an absorbing plane layer |

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absorbing medium bounded ABSORBING PLANE LAYER antisymmetry APPROXIMATE PREDICTIONS assumed to emit becomes available once black walls bounded by parallel D-2515 engineering design D-2515 National Aeronautics derive approxima dimensionless emission function employed to derive energy transport entire frequency range equa equation 12 equation l6 exponential function flux and temperature function see eq given whereby Heaslet and Franklyn interpolation formula iterative iterative methods Mass Transfer mean free path medium is assumed methods are employed Moffett Field NASA NASA TN once the problem optical depth optical thickness parallel walls previously published numerical Probstein published numerical results radiation isotropically radiative characteristics radiative flux radiative transport relations are given Simple formulas solution becomes available specific intensity stellar atmospheres TECHNICAL NOTE D-2515 thermal radiation thermodynamic equilibrium tions of radiative TN D-2515 engineering TN D-2515 National transmit the radiation transport of thermal Usiskin and Sparrow values walls are heated walls is solved whereby the solution