Development of high fidelity reduced order hybrid stick model for aircraft dynamic aeroelasticity analysis-Reference-Cited by-同舟云学术

Development of high fidelity reduced order hybrid stick model for aircraft dynamic aeroelasticity analysis

Published:2019-04 Issue: Volume:87 Page:404-416
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Vazhayil Thomas Paul,ElSayed Mostafa S.A.,Walch Denis

Funder

Bombardier

CARIC National Forum

MITACS

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference41 articles.

1. Monitor points method for loads recovery in static/dynamic aeroelasticity analysis with hybrid airframe representation;ElSayed;SAE Int. J. Aerosp.,2013

2. Accurate stick model development for static analysis of complex aircraft wing-box structures;ElSayed;AIAA J.,2009

3. Multilevel structural optimization for preliminary wing-box weight estimation;Bindolino;J. Aircr.,2010

4. Derivation of an equivalent beam model from a structural finite element model;Singh,1988

5. Impact of wing box geometrical parameters on stick model prediction accuracy;Corriveau,2013

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