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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Format: | Article |
Language: | English |
Published: |
CTU Central Library
2004-01-01
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Series: | Acta Polytechnica |
Subjects: | |
Online Access: | https://ojs.cvut.cz/ojs/index.php/ap/article/view/558 |