Study of Stress-Strain State of an Aircraft Body at Steering Loads

A design scheme is considered: a cylindrical shell, which is loaded concentrated through the frame. A classical mathematical model is used for the adopted calculation scheme. Based on the mathematical model, the initial problem is analytically solved and an effective algorithm for multiparameter sol...

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Veröffentlicht in:	Mechanics of solids 2020-05, Vol.55 (3), p.423-436
Hauptverfasser:	Vinogradov, Yu. I., Menkov, G. B.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft Algorithms Classical Mechanics Cylindrical shells Mathematical analysis Mathematical models Parametric statistics Physics Physics and Astronomy Steering Strain Stress-strain relationships
Online-Zugang:	Volltext
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