Melasangam Prashanth Kumar

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...