Preliminary Determination of Propeller Aerodynamic Characteristics for Small Aeroplanes

Preliminary Determination of Propeller Aerodynamic Characteristics for Small Aeroplanes

This paper deals with preliminary determination of propeller thrust and power coefficients depending on the advance ratio by means of some representative geometric parameters of the blade at a specific radius: propeller blade chord and blade angle setting at 70 % of the top radius, airfoil thickness...

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Bibliographic Details
Main Author: S. Slavík
Format: Article
Language:English
Published: CTU Central Library 2004-01-01
Series:Acta Polytechnica
Subjects:
propeller
propeller aerodynamics
thrust coefficient
power coefficient
propeller efficiency
propeller design
Online Access:https://ojs.cvut.cz/ojs/index.php/ap/article/view/558

Internet

https://ojs.cvut.cz/ojs/index.php/ap/article/view/558

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