The results calculation of the unstationary temperature field spherical and conical cowling aerial of head part perspective supersonic aircraft, heated during motion in the dense layers of atmosphere is offered. A method differs from known possibility of account sphericity and multi-layeredness construction, and also dependences properties of material on a temperature at all time flight of aircraft.
cowling, unstationary temperature field, aerodynamic heating, difficult heat exchange, grid model
"Rezultatы rascheta nestatsyonarnoho temperaturnoho polia razlychnыkh form obtekatelei antennы perspektyvnыkh sverkhzvukovыkh letatelnыkh apparatov" ,
Information Processing Systems,