The method calculation of the unstationary temperature field spherical 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
"Metod rascheta nestatsyonarnoho temperaturnoho polia sferycheskoho obtekatelia antennы perspektyvnыkh sverkhzvukovыkh letatelnыkh apparatov" ,
Information Processing Systems,