Propeller Aerodynamic Analyses by Vortex-Lattice Mathod, Part 2: Aerodynamic Parameters, Application

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001093" target="_blank" >RIV/00010669:_____/10:#0001093 - 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

Propeller Aerodynamic Analyses by Vortex-Lattice Mathod, Part 2: Aerodynamic Parameters, Application

Original language description

Described Vortex Lattice Method (VLM) analytical model calculates a field of induced velocities along propeller radius and simultaneously along blade airfoils chord. Aerodynamic forces and moments of the forces acting on single propeller elements are developed in the article. These do for summation propeller aerodynamic coefficients and local ones assessment. The analyses are verified with the aid of two model propellers. Graphic results of circulation distribution, induced velocity components and aerodynamic coefficient dependencies are presented.

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

<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

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

1/2010

Issue of the periodical within the volume

1

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

11

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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