Determination of Twin Turboprop Utility Aircraft Whirl Flutter stability Boundaries

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001553" target="_blank" >RIV/00010669:_____/10:#0001553 - isvavai.cz</a>

Result on the web

<a href="http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/" target="_blank" >http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Determination of Twin Turboprop Utility Aircraft Whirl Flutter stability Boundaries

Original language description

The submitted paper deals with the aircraft structure whirl flutter analysis. It gives a summary of the regulations requirements, the theoretical background and the aircraft certification relating issues. The main part deals with the whirl flutter analyses of the new twin turboprop utility aircraft. The optimization based analytical procedure to determine the whirl flutter stability boundaries for the certification speed is employed. Finally, the propeller ? nacelle - wing interference effects (downwash) are evaluated and the future work is outlined

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2010

Confidentiality

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

Article name in the collection

ICAS 2010 Proceedings

ISBN

978-0-9565333-0-2

ISSN

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e-ISSN

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Number of pages

10

Pages from-to

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Publisher name

The International Council of the Aeronautical Sciences (ICAS)

Place of publication

Francie

Event location

Nice, Francie

Event date

Jan 1, 2010

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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