FORMULACE MATRIX PRO VÝPOČET ROZLOŽENÍ ZATÍŽENÍ KŘÍDLA

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F06%3APU62720" target="_blank" >RIV/00216305:26210/06:PU62720 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

MATRIX FORMULATION FOR CALCULATIONS OF WING LOADING DISTRIBUTION

Popis výsledku v původním jazyce

An aeroplane is influenced by wide spectrum of loads during operations. The spectrum of loads is given by flight and landing load cases, mass and operation configurations leading to a great number of load cases that all have to be taken into consideration for loading of an aeroplane. The automation of computation is necessary and cannot be done without modification of the computation methodology. The paper describes the process of wing loading computation using a matrix formulation. This formulation simplifies the solution of complicated and time consuming dynamic loading, caused by numerical methods, and enables the selection of the essential loads in a uniform data basis. Explanation is based on an example of a wing loading. The method, described inthis paper, was successfully applied in the CAE system for aeroplane loading computation, named SAVLE (System for Automation of Load Calculation of Aeroplanes), which was used in Czech aircraft industry during the development of several a

Název v anglickém jazyce

MATRIX FORMULATION FOR CALCULATIONS OF WING LOADING DISTRIBUTION

Popis výsledku anglicky

An aeroplane is influenced by wide spectrum of loads during operations. The spectrum of loads is given by flight and landing load cases, mass and operation configurations leading to a great number of load cases that all have to be taken into consideration for loading of an aeroplane. The automation of computation is necessary and cannot be done without modification of the computation methodology. The paper describes the process of wing loading computation using a matrix formulation. This formulation simplifies the solution of complicated and time consuming dynamic loading, caused by numerical methods, and enables the selection of the essential loads in a uniform data basis. Explanation is based on an example of a wing loading. The method, described inthis paper, was successfully applied in the CAE system for aeroplane loading computation, named SAVLE (System for Automation of Load Calculation of Aeroplanes), which was used in Czech aircraft industry during the development of several a

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

<a href="/cs/project/1M0501" target="_blank" >1M0501: Centrum leteckého a kosmického výzkumu</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2006

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

CD PROCEEDINGS

ISBN

0-9533991-7-6

ISSN

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e-ISSN

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Počet stran výsledku

6

Strana od-do

1-6

Název nakladatele

Optimage Ltd., Edinburgh, UK

Místo vydání

HAMBURG, GERMANY

Místo konání akce

Hamburg

Datum konání akce

3. 9. 2006

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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