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Optimized Design Methodology for Wing Box Structures Utilizing Euler–Bernoulli Beam Theory

  • Beihang University
  • Ohio State University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Accurate wing box weight estimation is critical in early aircraft design. Traditional empirical methods lack precision for novel configurations, while high-fidelity finite element analysis (FEA) is computationally intensive. This study presents a rapid, robust estimation framework based on Euler–Bernoulli beam theory. The method parameterizes wing box geometry via spar locations, computes cross-sectional properties, and evaluates structural response under typical loads. Strength and buckling stability checks ensure structural reliability. Validation against FEA under identical conditions achieved the intended objectives in terms of engineering applicability. This approach offers an efficient and accurate tool for preliminary wing box structural weight assessment, facilitating early-stage design decisions.

Original languageEnglish
Title of host publicationMoving Integrated Product Development to Service Clouds in the Global Economy - Proceedings of the 21st ISPE Inc. International Conference on Concurrent Engineering, CE 2014
EditorsXuelin Lei
PublisherIOS Press BV
Pages400-409
Number of pages10
ISBN (Electronic)9781643686479
DOIs
StatePublished - 3 Mar 2026
Event16th International Conference of Mechanical and Aerospace Engineering, ICMAE 2025 - Rome, Italy
Duration: 15 Jul 202518 Jul 2025

Publication series

NameAdvances in Transdisciplinary Engineering
Volume87
ISSN (Print)2352-751X
ISSN (Electronic)2352-7528

Conference

Conference16th International Conference of Mechanical and Aerospace Engineering, ICMAE 2025
Country/TerritoryItaly
CityRome
Period15/07/2518/07/25

Keywords

  • Euler–Bernoulli beam theory
  • genetic algorithm
  • stability check
  • strength check
  • wing box mass estimation

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