Wind tunnel tests of oscillating wing using the surface pressure transducers.

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230000998" target="_blank" >RIV/00010669:_____/10:#0000998 - 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

Wind tunnel tests of oscillating wing using the surface pressure transducers.

Original language description

This article deals with aerodynamic measurement of oscillated wing model AS28 with newly installed surface pressure transducers KULITE. In the frame of this work the practical task of the test of new technology of the surface pressure measurement and verifying of early results measured on this model was realized. There is introduced the development of unsteady measurement on the oscillated half-wing model in high speed laboratory of VZLU, the measurement, results and comparison of used methods.

Czech name

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Czech description

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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

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Continuities

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2010

Confidentiality

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

Name of the periodical

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

4/2010

Issue of the periodical within the volume

4

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

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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