Aerodynamic characteristics of wing having spanwise camber

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F14%3A00236650" target="_blank" >RIV/68407700:21220/14:00236650 - isvavai.cz</a>

Result on the web

<a href="http://stc.fs.cvut.cz/history/2014/sbornik/papers/pdf/4524.pdf" target="_blank" >http://stc.fs.cvut.cz/history/2014/sbornik/papers/pdf/4524.pdf</a>

DOI - Digital Object Identifier

—

Result language

angličtina

Original language name

Aerodynamic characteristics of wing having spanwise camber

Original language description

This paper deals with problematics of wings having spanwise chamber. The numerical method based on philosophy of Prandtl's lifting lines theory is derived in first part of this paper. This method allows analysis of spatial chambered wings. Influence of spanwise chamber on aerodynamic characteristics is discussed in following chapter. In the last part of this paper an author focus to possible extension of presented method.

Czech name

—

Czech description

—

Type

D - Article in proceedings

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

—

Project

—

Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2014

Confidentiality

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

Article name in the collection

STČ 2014

ISBN

978-80-01-05484-0

ISSN

—

e-ISSN

—

Number of pages

8

Pages from-to

-1

Publisher name

ČVUT, Fakulta strojní

Place of publication

Praha

Event location

Praha

Event date

Apr 8, 2014

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

—