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 exchang
"Obosnovanye znachenyia ploshchady dostovernoho porazhenyia tselei sredstvamy porazhenyia, osnashchennыmy oskolochno-fuhasnыmy boeprypasamy" ,
Science and Technology of the Air Force of Ukraine,