Simulation of propeller effect in wind tunnel

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F16%3AN0000121" target="_blank" >RIV/00010669:_____/16:N0000121 - isvavai.cz</a>

Result on the web

<a href="http://www.icas.org/ICAS_ARCHIVE/ICAS2016/data/papers/2016_0593_paper.pdf" target="_blank" >http://www.icas.org/ICAS_ARCHIVE/ICAS2016/data/papers/2016_0593_paper.pdf</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Simulation of propeller effect in wind tunnel

Original language description

Significance of the influence of operating propellers on aircraft aerodynamic characteristics is well-known. Wind tunnel testing of an aeroplane model with operating propellers is a complex task regarding the required similarity of the full-scale and the model case. Matching sufficient similarity in axial and rotational velocities in the propeller slipstream is the primordial condition for theglobal aerodynamic similarity of the wind tunnel testing. An example of the model power units with related devices is presented. Examples of the wind tunnel testing results illustrate the extent of propeller influence on aerodynamic characteristics of a generic aircraft.

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

6

Pages from-to

1-6

Publisher name

International Council of the Aeronautical Sciences

Place of publication

Německo

Event location

Daejeon, Jižní Korea

Event date

Sep 25, 2016

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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