Method for calculating lateral bending rigidity of section of airframe door frame area of airframe

A method for calculating the lateral bending rigidity of the section of an aircraft fuselage door frame area comprises the steps that design parameters of an aircraft fuselage and a door frame are known, the parameters comprise the fuselage skin thickness, the fuselage radius, the cross section area...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZHANG ZENGGUANG, YIN KAIJUN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
Online-Zugang:	Volltext bestellen
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