Aerodynamic Design and Optimization of Single Slotted Flap

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F03%3APU36643" target="_blank" >RIV/00216305:26210/03:PU36643 - 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

Aerodynamic Design and Optimization of Single Slotted Flap

Original language description

The method for aerodynamic design and optimization of single slotted flap is presented. As a tool for preliminary design of flap shape a panel method is used. The flap position in the landing configuration is optimized. The Nelder-Mead simplex method isused as optimization algorithm. The aerodynamic performance is predicted using commercial CFD software Fluent 6. The design/optimization approach is first validated by calculation of NACA 23012 airfoil with single slotted flap and by comparing with expperimental investigation. Results show the appropriateness of the approach for design and optimization of single slotted flap.

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

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

2003

Confidentiality

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

Name of the periodical

AVIATION

ISSN

1648-7788

e-ISSN

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Volume of the periodical

7

Issue of the periodical within the volume

3

Country of publishing house

LT - LITHUANIA

Number of pages

4

Pages from-to

45-48

UT code for WoS article

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EID of the result in the Scopus database

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