Evolution by Trial and Error

SM_VSTOL_1972-2653

10/26/1972

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Abstract
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It has been said that when you encounter a native from Holland he will talk about windmills within five minutes. So, what else is there for me to do in the seven minutes I am given by the chairman? The windmill I visited last year had a large rigid rotor of about 100 feet diameter and was built in 1648. its four blades incorporated nonlinear twist and a thin droopsnoot airfoil near the blade tip (see Fig. 1). The mast angle could he adjusted to relieve the hub moments and to prevent overspeeding. (This was done manually, although techniques were available to do it automatically with a tail rotor.) Flutter was avoided in the wide-chord blades (solidity .2) by locating the main spar and the blade c.g. at the quarter-chord point. The development of this rotor system had taken a little while – in fact, about 400 years – by evolution through the process of trial and error.

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DOI
https://doi.org/10.4050/SM_VSTOL_1972-2653
Citation
Drees, J., "Evolution by Trial and Error," Symposium on Status of Testing and Modeling Techniques for V/STOL Aircraft, Philadelphia 1972, Philadelphia, Pennsylvania, October 26, 1972, https://doi.org/10.4050/SM_VSTOL_1972-2653.
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Publisher
Published
10/26/1972
Product Code
SM_VSTOL_1972-2653
Content Type
Technical Paper
Language
English