DESIGN OF COMPOSITE STRUCTURE OF A SMALL AIRCRAFT USING FEM ANALYSIS
Identifikátory výsledku
Kód výsledku v 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>
Výsledek na webu
—
DOI - Digital Object Identifier
—
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
DESIGN OF COMPOSITE STRUCTURE OF A SMALL AIRCRAFT USING FEM ANALYSIS
Popis výsledku v původním jazyce
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.
Název v anglickém jazyce
DESIGN OF COMPOSITE STRUCTURE OF A SMALL AIRCRAFT USING FEM ANALYSIS
Popis výsledku anglicky
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.
Klasifikace
Druh
O - Ostatní výsledky
CEP obor
JU - Aeronautika, aerodynamika, letadla
OECD FORD obor
—
Návaznosti výsledku
Projekt
<a href="/cs/project/ED0002%2F01%2F01" target="_blank" >ED0002/01/01: NETME Centre (Nové technologie pro strojírenství)</a><br>
Návaznosti
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Ostatní
Rok uplatnění
2016
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů