INFLUENCE OF ICE ACCRETIONS ON AERODYNAMIC PERFORMANCE OF AIRFOIL

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F09%3A%230000921" target="_blank" >RIV/00010669:_____/09:#0000921 - 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

INFLUENCE OF ICE ACCRETIONS ON AERODYNAMIC PERFORMANCE OF AIRFOIL

Original language description

An investigation was performed, by means of low-speed wind tunnel testing, to study the effect of different ice accretions on NASA MS(1)-0317 airfoil with Fowler flap. The cases studied covered very different icing conditions. The ice accretion was simulated by placing strips of different shapes in the region of expected accretion. The influence on basic aerodynamic characteristics and on pressure distributions was evaluated for each case. The potential consequences of the icing phenomenon at differentconditions to flight performance and consequently the safety of general aviation aircraft are evident.

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

R - Projekt Ramcoveho programu EK

Publication year

2009

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

3/2009

Issue of the periodical within the volume

3

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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