CFD Calculation of the Wing with High-lift Devices

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001018" target="_blank" >RIV/00010669:_____/10:#0001018 - 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

CFD Calculation of the Wing with High-lift Devices

Original language description

This article deals with the CFD calculation of the initial configuration of an airliner wing equipped with double slotted flap and modified leading edge (Fixed Droop Nose + Double Slotted Flap). No slat on the leading edge was used. Two deflections of the double slotted flap were calculated by EDGE program. This work is referring to previous article Grid Generation in ICEM CFD Software for CFD Calculation of Wing with High-lift Devices. The limitation of lift coefficient by Mach number was observed.

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

3/2010

Issue of the periodical within the volume

3

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

3

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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