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Stability and Control in Aircraft Design

Published online by Cambridge University Press:  28 July 2016

J. C. Wimpenny
J. C. Wimpenny*
Affiliation:
The de Havilland Aircraft Co. Ltd.
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Extract

The 890th Lecture to be given before the Royal Aeronautical Society was held at the Institution of Mechanical Engineers, Storey's Gate, London, S.W.I, on 12th November 1953, and was presided over by Sir William Farren, C.B., M.B.E., M.A., F.R.S., F.R.Ae.S., President of the Society. Introducing the lecturer, Sir William said that Mr. Wimpenny had been with the de Havilland Company throughout his career in aviation and had been responsible for some years for the design and development of stability and control of the de Havilland aircraft, including the Comet, so that clearly he spoke with a wide knowledge of his subject.

Type
Research Article
Information
The Aeronautical Journal , Volume 58 , Issue 521 , May 1954 , pp. 329 - 360
Copyright
Copyright © Royal Aeronautical Society 1954

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References

1. Gates, S. B. and Lyon, H. M. (1944). A continuation of longitudinal stability and control analysis. Part I, General Theory. R. & M. 2027. Part II, Interpretation of Flight Tests. R. & M. 2028.Google Scholar
2. Craik, K. J. W. (1948). Theory of the Human Operator in Control Systems. II—Man as an Element in a Control System. British Journal of Psychology, Vol. 38, Part 3, March 1948.Google Scholar
3. Milliken, W. Jr. (1951). Dynamic Stability and Control Research. Third Anglo-American Aeronautical Conference, Brighton. The Royal Aeronautical Society, 1952.Google Scholar
4. Hill, G. T. R. (1951). Advances in Aircraft Structural Design. Third Anglo-American Aeronautical Conference, Brighton. The Royal Aeronautical Society, 1952.Google Scholar