A Set Theoretic approach for reducing critical load cases in aircraft structural design

Aerospace Science and Technology 2026

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Authors: Ahmet Karaca, Ömer Onur
DOI: 10.1016/j.ast.2026.111826
Cited by: 0
References: 7

Fields of Study & Subjects

Aeroelasticity and Vibration Control Advanced Aircraft Design and Technologies Engineering Applied Research

Publication details

Journal / source
Aerospace Science and Technology
Volume
174
Pages
111826–111826
Publication date
4 February 2026
Language
EN