Experimental and computational study of ground effect on airfoil section

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F16%3AN0000103" target="_blank" >RIV/00010669:_____/16:N0000103 - isvavai.cz</a>

Result on the web

<a href="http://icas.org/ICAS_ARCHIVE/ICAS2016/data/papers/2016_0122_paper.pdf" target="_blank" >http://icas.org/ICAS_ARCHIVE/ICAS2016/data/papers/2016_0122_paper.pdf</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Experimental and computational study of ground effect on airfoil section

Original language description

The influence of ground proximity on aerodynamic characteristics of an airfoil was studied at low Reynolds number. The study, motivated mainly by sailplane take-off and landing safety, provides information about the development of the pressure distributions and of the aerodynamic forces acting on the airfoil with the approaching of the airfoil to the ground. Differences caused by fixed or by moving ground were examined using CFD computations.

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

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2016

Confidentiality

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

Article name in the collection

ICAS 2016 - CD-ROM PROCEEDINGS

ISBN

978-3-932182-85-3

ISSN

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e-ISSN

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Number of pages

8

Pages from-to

1-8

Publisher name

International Council of the Aeronautical Sciences

Place of publication

Neuveden

Event location

Daejeon, Korea

Event date

Sep 25, 2016

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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