Vertical tail FEA with a CAD/CAE based multidisciplinary process

Péter Deák (Department of Aircraft Design, Politechnika Warszawska, Warsaw, Poland)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Publication date: 8 May 2018

Abstract

Purpose

The purpose of this paper is to make an analytical comparison of two vertical tail models from a structural point of view.

Design/methodology/approach

The original vertical tail design of PZL-106BT aircraft was used for Computer aided design (CAD) modeling and for creating the finite element model.

Findings

The nodal displacements, Von-Mises stresses and Buckling factors for two vertical tail models have been found using the finite element method. The idea of a possible Multidisciplinary concept assessment and design (MDCAD) concept was presented.

Practical implications

The used software analogy introduces an idea of having an automated calculation procedure within the framework of MDCAD.

Originality/value

The aircraft used for calculation had undergone a modification in its vertical tail length, as there was an urgent need to calculate for the plane’s manufacturer, PZL Warszawa – Okecie.

Keywords

Citation

Péter Deák (2018) "Vertical tail FEA with a CAD/CAE based multidisciplinary process", Aircraft Engineering and Aerospace Technology, Vol. 90 No. 4, pp. 652-658

Download as .RIS

DOI

: https://doi.org/10.1108/AEAT-11-2016-0212

Publisher

:

Emerald Publishing Limited

Copyright © 2018, Emerald Publishing Limited

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