The paper considers a conical shell of the head fairing of a hypersonic aircraft that is connected through the frame with the cylindrical shell. Possibilities of reducing the maximum stresses at the connection are analyzed.
A Technique of Stress Reduction in a Conical Shell of the Head Radio-Transparent Fairing of the Aircraft
Russ. Aeronaut.
Russian Aeronautics ; 63 , 3 ; 377-385
2020-09-01
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
WEDGE-SHAPED RADIO-TRANSPARENT FRONT FAIRING OF THE SUPERSONIC AIRCRAFT CASE
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