ESTIMATION OF WEIGHT REDUCTION IN AIRCRAFT WING RIB

Authors:

Dr. Ch Mallikarjun, Mr.Shaik Meravali

Page No: 251-258

Abstract:

The estimation of weight reduction in aircraft wing ribs is a critical aspect of modern aerospace engineering, focusing on the optimization of material usage and structural integrity. Aircraft wing ribs are essential components of the wing structure, providing support to the wing skin and contributing to the overall strength of the wing. Traditionally, the materials used for these ribs have been selected based on strength and durability considerations, but these solutions often result in heavier components that negatively impact the aircraft's fuel efficiency and overall performance

Description:

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Volume & Issue

Volume-13,ISSUE-11

Keywords

Aircraft wing ribs, weight reduction, structural optimization, composite materials, finite element analysis (FEA), design alternatives.

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