Aeroelastic tailoring for aerospace applications.

Aeroelastic optimization Aeroelastic tailoring Aeroelasticity Aerospace applications Flutter mitigation Passive aeroelastic control

Journal

Heliyon
ISSN: 2405-8440
Titre abrégé: Heliyon
Pays: England
ID NLM: 101672560

Informations de publication

Date de publication:
30 Jan 2024
Historique:
received: 02 09 2023
revised: 05 12 2023
accepted: 04 01 2024
medline: 31 1 2024
pubmed: 31 1 2024
entrez: 31 1 2024
Statut: epublish

Résumé

This study presents a brief account of the seminal works on aeroelastic tailoring for aerospace applications. Tailoring using advanced composites is a revolutionary process in the ever-evolving realm of aerospace design. The rapid growth in scientific knowledge and research necessitates the consolidation of the latest research and technological advancements every few years. The current work is part of this process. The major portion of the study covers the latest developments and state-of-the-art research in this century, with a special focus on the last ten years. However, a brief account of the historical background, the theoretical foundation, and a few seminal works from the later part of the previous century and the early part of this century have also been included to form a comprehensive starting point for new researchers entering the field of aeroelastic tailoring and to assist them in identifying the directions of their future endeavours. A critical evaluation of different research contributions, including their advantages, limitations, and prospects for future work, has been presented. Emphasis has been laid on flutter mitigation and aeroelastic optimization for passive aeroelastic control. New material and structural technologies (like curvilinear fibres, tow steering, functional grading, thickness distributions, selective reinforcing, additive manufacturing, and unconventional structural configurations), and novel tailoring optimization techniques (like lamination parameters, blending constraints, active aeroelastic wing design, shape functions, surrogate modelling, reduced order modelling, uncertainty quantification, matrix perturbation theory, modal-strain-energy analyses, and multiple indigenous optimization algorithms) have been identified as active research areas and prospective enabling tools for future work. The challenges faced in the full-scale employment of aeroelastic tailoring include quick, robust, and cost-effective optimization to cater for all design variables and constraints, experimental validation of new methodologies, certification of new material and structural configurations through relevant bodies and standards and gaining the confidence of industrialists for investment in technologies with a few highly focused areas of applications.

Identifiants

pubmed: 38293373
doi: 10.1016/j.heliyon.2024.e24151
pii: S2405-8440(24)00182-8
pmc: PMC10825427
doi:

Types de publication

Journal Article Review

Langues

eng

Pagination

e24151

Informations de copyright

© 2024 The Authors.

Déclaration de conflit d'intérêts

The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

Auteurs

Junaid Najmi (J)

Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology (NUST), Pakistan.

Haris Ali Khan (HA)

Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology (NUST), Pakistan.

Syed Saad Javaid (SS)

Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology (NUST), Pakistan.

Asad Hameed (A)

Department of Aerospace Engineering, College of Aeronautical Engineering, National University of Sciences and Technology (NUST), Pakistan.

Faisal Siddiqui (F)

Department of Aerospace Engineering, Air University Aerospace and Aviation Campus, Kamra, Pakistan.

Classifications MeSH