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Abstracts from the Scientific and Technical Press

Published online by Cambridge University Press:  28 July 2016

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Abstract

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Information
The Aeronautical Journal , Volume 41 , Issue 322 , October 1937 , pp. 953 - 970
Copyright
Copyright © Royal Aeronautical Society 1937

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References

* Effectiveness of the control surface is denned by the authors as the constant angular velocity imparted to the aeroplane, when flying at minimum speed, for an aileron angular velocity of 1 radian/sec.