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Open access Jul 2026

The Design and Finite Element Analysis of a Titanium Alloy, Structural Steel, and Grey Cast Iron Aircraft Fuselage Skin Panel

The skin panel of the fuselage is one of the main parts of a transport plane's semi-monocoque airframe that bears the weight of the plane and must be as lightweight as possible while still withstanding cabin pressurization loads, inertia loads while in flight, and compressive loading caused by the plane bending without...

K. Vaibhav, B. Rani · 0 citations
Open access Jul 2026

A Comparison of CATIA V5 and ANSYS for the Design and Finite Element Analysis of a Standard Wing Rib for Passenger Aircraft

Under flight stress, an aircraft wing's aerodynamic shape shouldn't deform too much, and the skin-stringer panels shouldn't buckle locally under compressive force if the wing is supported at close enough intervals. During normal flight, the wing ribs—which are transverse structural members—meet these requirements by ma...

Melasangam Prashanth Kumar, P. R. Raju, B. Rani · 0 citations

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