Wind Tunnel Simulation of Ice Accretion on Tail Unit

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F02%3A00007051" target="_blank" >RIV/00010669:_____/02:00007051 - 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 Simulation of Ice Accretion on Tail Unit

Original language description

An experimental investigation was conducted to study the aerodynamic effect of simulated ice accretion on a wing and horizontal tailplane of an aircraft by means of wind tunnel testing. The strips simulating both a conventional leading-edge accretion andice accretion caused by supercooled large droplets were used. Its influence on the basic aerodynamic characteristics of the aircraft was evaluated, i.e. lift, drag, side force and moments.

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

<a href="/en/project/OK%20438" target="_blank" >OK 438: ProfeSsional Contact Organization - Aviation and Space Research</a><br>

Continuities

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

Publication year

2002

Confidentiality

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

Article name in the collection

Proceedings of 23rd International Congress of Aeronautical Sciences

ISBN

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ISSN

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e-ISSN

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Number of pages

6

Pages from-to

23-28

Publisher name

ICAS

Place of publication

Toronto

Event location

Toronto

Event date

Jan 1, 2002

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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