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2020 | OriginalPaper | Buchkapitel

8. Experiments

verfasst von : A. P. Schaffarczyk

Erschienen in: Introduction to Wind Turbine Aerodynamics

Verlag: Springer International Publishing

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Abstract

As we have explained extensively in the previous chapters the blade-element-momentum method describes blades—aerodynamically—as a set of independent 2D airfoils. Therefore, wind tunnel measurement of 2D sections is the basis of all aerodynamical experiments for wind turbines. Fortunately, a lot of experience has been gained for airfoils of airplanes which could be used when special airfoils started to be designed [33] in Chap. 9.

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Fußnoten
1
This code is comparable to the so-called Eppler-code [17] in Chap. 3, developed somewhat earlier and was extended to include 3D-effect from stall-delay for rotation in [32].
 
2
Roughly speaking this is the ratio where a small disturbance has grown to a relevant size.
 
3
In [15, 16] even a much lager range of \(\nu < 500\) Hz is excluded.
 
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Metadaten
Titel
Experiments
verfasst von
A. P. Schaffarczyk
Copyright-Jahr
2020
DOI
https://doi.org/10.1007/978-3-030-41028-5_8