PIV Investigation of an High-Performance Airfoil with a Gurney Flap

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F05%3A02113448" target="_blank" >RIV/68407700:21220/05:02113448 - 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

PIV Investigation of an High-Performance Airfoil with a Gurney Flap

Original language description

This paper reviews the research on FX 66-17AII-182 airfoil profile equipped with Gurney flap. It investigates airfoil performances for different angles of attack at effective Reynolds number, based on chord, with clean configuration, Gurney flap, vortexgenerator and combination of Gurney flap and vortex generator. Measuring device 2D-PIV (Two-dimensional Particle Image Velocimetry) system was used.

Czech name

Měření vztlaku profilu křídla s Gurneyho klapkou metodou PIV

Czech description

Článek popisuje výzkum profilu křídla FX 66-17AII-182 s Gurneyho klapkou. Je zjišťován vztlak profilu křídla pro různé úhly náběhu.

Type

A - Audiovisual production

CEP classification

BK - Liquid mechanics

OECD FORD branch

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Project

Result was created during the realization of more than one project. More information in the Projects tab.

Continuities

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

Publication year

2005

Confidentiality

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

ISBN

1-930746-02-4

Place of publication

Sydney

Publisher/client name

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Version

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Carrier ID

neuvedeno