A robust and reliability-based aeroelastic tailoring framework for composite aircraft wings-Reference-Cited by-同舟云学术

A robust and reliability-based aeroelastic tailoring framework for composite aircraft wings

Published:2019-01 Issue: Volume:208 Page:101-113
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Othman Muhammad F.,Silva Gustavo H.C.,Cabral Pedro H.,Prado Alex P.,Pirrera Alberto^ORCID,Cooper Jonathan E.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference44 articles.

1. Aeroelastic tailoring of composite structures;Eastep;J Aircraft,1999

2. Kuzmina S, Chedrik V, Ishmuratov F. Strength and aeroelastic structural optimization of aircraft lifting surfaces using two-level approach. In 6th world congress of structural and multidisciplinary optimization.

3. Multi-objective optimization of a composite wing subject to strength and aeroelastic constraints;Guo;Proc Inst Mech Eng Part G,2011

4. Stiffness optimization of composite wings with aeroelastic constraints;Dillinger;J Aircraft,2013

5. Herencia JE, Weaver PM, Friswell MI. Morphing wing design via aeroelastic tailoring. In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference; 2007. pp. 1–19.

Cited by 16 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Quantile-based optimization under uncertainties for complex engineering structures using an active learning basis-adaptive PC-Kriging model;Chinese Journal of Aeronautics;2024-08

2. Development of a Nonlinear Structural Stability Constraint for Aeroelastic Optimization;AIAA SCITECH 2024 Forum;2024-01-04

3. Aeroelastic Tailoring Framework of Pazy Wing With Variable Stiffness of Composites Spar;IEEE Access;2024

4. Aeroelastic tailoring for aerospace applications;Heliyon;2024-01

5. Investigation of Limit Cycle Oscillations and Phase Portraits in Gfrp Based Composite Structures Embedded with Superelastic Shape Memory Alloy Wires;2024