Measurement of the Wing Bending Moment of Aircraft CS-23 Category

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F08%3APU79299" target="_blank" >RIV/00216305:26210/08:PU79299 - 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

Measurement of the Wing Bending Moment of Aircraft CS-23 Category

Original language description

The goal of measurement was to set curves of bending moment on the wing of a small aircraft CS-23 category. The producer of the aircraft firstly installed a set of strain gauges and after this their calibration procedure was done. Basic parameters such as, speed, flight load factor, altitude and electrical response of strain gages were recorded by the data acquisition system ESAM Static. The measured responses were analyzed and calculated bending moments were compared with the computed results.

Czech name

Měření ohybových momentů letounu kategorie CS-23

Czech description

Článek pojednává o měření ohybových momentů na letounu kategorie CS-23

Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

<a href="/en/project/1M0501" target="_blank" >1M0501: Aerospace Research Centre</a><br>

Continuities

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

Publication year

2008

Confidentiality

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

Name of the periodical

Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

2008

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

10

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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