Response Surface Method Application to Transonic Business-jet Wing Optimization

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F10%3APU86868" target="_blank" >RIV/00216305:26210/10:PU86868 - isvavai.cz</a>

Result on the web

—

DOI - Digital Object Identifier

—

Result language

angličtina

Original language name

Response Surface Method Application to Transonic Business-jet Wing Optimization

Original language description

The article gives overview of complex aerodynamic optimization approach applied to business-jet aircraft wing design. In the frame of 6th EU FP integrated project CESAR [1] generic business-jet configuration was designed and diverse optimization techniques were applied to airfoil and wing design by members of project consortium. The authors explored particularly response surface method (RSM) potential for global wing aerodynamic optimization. The capability of method to support designer's decisions wasassessed and attempt to incorporate basic structural criteria in aerodynamic optimization was made.

Czech name

—

Czech description

—

Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

—

Project

<a href="/en/project/1M0501" target="_blank" >1M0501: Aerospace Research Centre</a><br>

Continuities

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

Publication year

2010

Confidentiality

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

Name of the periodical

Letecký zpravodaj

ISSN

1211-877X

e-ISSN

—

Volume of the periodical

2010

Issue of the periodical within the volume

1

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

5

Pages from-to

—

UT code for WoS article

—

EID of the result in the Scopus database

—