DESIGN OF COMPOSITE STRUCTURE OF A SMALL AIRCRAFT USING FEM ANALYSIS
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F16%3APU123033" target="_blank" >RIV/00216305:26210/16:PU123033 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
DESIGN OF COMPOSITE STRUCTURE OF A SMALL AIRCRAFT USING FEM ANALYSIS
Original language description
The article describes finite element method (FEM) utilization at lightweight structure design of a small aircraft made from composite material. The procedure begins at suitable material definition based on selected manufacturing technologies. Following problem presents an effective modeling of the structure. Evaluation of the simulation is presented as a key phase of the methodology. An open source freeware code ComPost has been written on the background of the small aircraft development projects. The code offers detailed post-processing of a composite laminates analyzed by finite elements method. A case study of the ComPost application at aircraft structure analysis of a VUT 081 Kondor demonstrates benefits of this code during a design phase of a small aircraft development.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
<a href="/en/project/ED0002%2F01%2F01" target="_blank" >ED0002/01/01: NETME Centre (New Technologies for Mechanical Engineering)</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů