STUDY OF THE AIRCRAFT CONICAL FAIRING DYNAMIC BEHAVIOUR UNDER COMBINED OF TEMPERATURE AND FORCE LOADING

STUDY OF THE AIRCRAFT CONICAL FAIRING DYNAMIC BEHAVIOUR UNDER COMBINED OF TEMPERATURE AND FORCE LOADING

The article deals with the dynamic behavior of the unevenly heated thin-walled conical shell of revolution of the aircraft fairing type under the loading conditions by shock wave in the gaseous environment, approximated by travelling load. The displacements of the shell, resulting from the prelimina...

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Bibliographic Details
Main Authors: I. K. Turkin, D. A. Rogov
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-12-01
Series:Научный вестник МГТУ ГА
Subjects:
обтекатель
оболочка
летательный аппарат
термосиловое нагружение
Online Access:https://avia.mstuca.ru/jour/article/view/891

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