Facility Developement for Frequency Tests of Small Aeroplanes

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F03%3A02091382" target="_blank" >RIV/68407700:21220/03:02091382 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Facility Developement for Frequency Tests of Small Aeroplanes

Original language description

This paper presents the laboratory dynamic device for frequency tests of small aeroplanes and gliders up to the maximum takeoff weight 650 kg. The equipment is developed in terms of the task Research Development of Aircraft Composite Structures of the project Aerospace Research Centre. The method described deals with critical flutter speeds of small aeroplanes and gliders as a base of the device design and measurement methodology. This article gives information of a measuring Unit of the equipment and characteristics of separate hardware components. Suspension structure is presented. A schematic form of the measurement methodology is mentioned.

Czech name

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Czech description

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Type

A - Audiovisual production

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>

Continuities

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

Publication year

2003

Confidentiality

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

ISBN

80-86059-35-9

Place of publication

Praha

Publisher/client name

Not available

Version

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Carrier ID

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