Shielding Of Partially Reflecting Stagnation Surfaces Against Radiation By Transpiration Of An Absorbing Gas
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Shielding of Partially Reflecting Stagnation Surfaces Against Radiation by Transpiration of an Absorbing Gas
The laminar compressible boundary layer in the two dimensional and axisymmetric stagnation regions has been analyzed to show the effects of the injection of a radiation absorbing gas on the incident radiation field, on enthalpy profiles, and on heat transfer to the vehicle surface. Heat-transfer results are presented and are compared with those for the unshielded case. The required absorption properties of the foreign gas are determined and compared with properties of known gases.