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Helicopter Stability in Hovering Flight

Published online by Cambridge University Press:  28 July 2016

K. H. Hohenemser
K. H. Hohenemser*
Affiliation:
Helicopter Engineering Division, McDonnell Aircraft Corporation, U.S.A.
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Abstract

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Type
Technical Notes
Information
The Aeronautical Journal , Volume 60 , Issue 548 , August 1956 , pp. 550 - 553
Copyright
Copyright © Royal Aeronautical Society 1956

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References

1. Rogers, V. A. B. (1955). Letter to the Editor Aircraft Engineering. Vol. XXVII, No. 319. September 1955.Google Scholar
2. Price, H. L. (1955). Letter to the Editor Aircraft Engineering Vol. XXVII No. 321 November 1955.Google Scholar
3. Payne, P. R. (1955). The Control of Helicopter Rotor Vibration. Lecture read before the Helicopter Association of Great Britain on October 7th 1955.Google Scholar
4. Payne, P. R. (1955). Helicopter Rotor Vibration in the Tip-path-plane. Aircraft Engineering, Vol. XXVII, No. 316, June 1955.Google Scholar
5. Miller, R. H. (1948). Helicopter Control and Stability in Hovering Flight. Journal of the Aeronautical Sciences, August 1948.Google Scholar
6. Payne, P. R. (1955). The Stiff-hinged Helicopter Rotor. Aircraft Engineering, Vol. XXVII No. 321 November 1955.Google Scholar
7. Robertson, F. H. (1955). Letter to the Editor Flight, p. 849, December 2nd 1955.Google Scholar