Hostname: page-component-586b7cd67f-t7czq Total loading time: 0 Render date: 2024-11-27T09:58:26.467Z Has data issue: false hasContentIssue false
  • English
  • Français

The Control of Helicopter Rotor Vibration

Published online by Cambridge University Press:  26 October 2023

P R Payne
P R Payne*
Affiliation:
Engine Division of the Bristol Aeroplane Company

Extract

Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.

The Chairman said the subject was of paramount importance to all helicopter designers, manufacturers and operators The Association had not previously had a lecture which dealt specifically with the problem and the importance of the subject meant that such a lecture was long overdue They knew that, in spite of the claims made from time to time by sundry manufacturers, helicopters did vibrate, some to a very great extent Indeed, one eminent fixed wing designer thought that by virtue of this vibration helicopters were rather more grandiose fatigue testing machines than the conventional test equipment for the purpose

Type
Research Article
Information
The Journal of the Helicopter Association of Great Britain , Volume 9 , Issue 3 , January 1956 , pp. 327 - 360
Copyright
Copyright © Royal Aeronautical Society 1956

References

P R Payne “Helicopter Rotor Vibration in the Tip-path Plane” Aircraft Engineering June, 1955CrossRefGoogle Scholar
W Stewart “Higher Harmomcs of Flappmg on the Helicopter Rotor” R A E Report Aero 2459Google Scholar
R Hafner “Simulation of Helicopter Operating Condltlons in Ground Tests” April, 1953, Issue of the Journal of the Helicopter AssociationGoogle Scholar
P R Payne “The Flight Envelope of a Helicopter” Journal of the Royal Aeronautical Society November, 1954CrossRefGoogle Scholar
R M Howarth & C H Jones “Ground Resonance of the Helicopter” Journal of the Helzcopter Association Vol 7, No 4 April, 1954Google Scholar
R Hafner “Rotor Systems and Control Problems in the Helicopter” Paper read before the Anglo-American Aeronautical Conference September 5th, 1947Google Scholar
J A Cameron “Recent Helicopter Flight Testmg Expenence” Journal of the Helicopter Association Vol 7, No 1 July, 1953Google Scholar
R Hafner “The Domam of the Helicopter” Journal of the Royal Aeronautical Society Vol 58, No 526 Oct, 1954CrossRefGoogle Scholar
P R Payne “Hub Moments and Forces of a High Offset Rotor” Aircraft Engineering January, 1955CrossRefGoogle Scholar
R P Coleman and C W Stempin “A Prelimmary Theoretical Study of Aerodynamic Instability of a Two-Blade Helicopter Rotor” N A C A RM L6H23, 1946Google Scholar
P R Payne “A General Theory of Helicopter Rotor Dynamics” August, 1954, issue of Aircraft EngineeringCrossRefGoogle Scholar
P R Payne “A Rapid Method of Estimatmg Propeller Moment” April, 1954, issue of Journal of Royal Aeronautical Society Addendum in December, 1954, issueCrossRefGoogle Scholar
Ken Williams “Fatigue Life of Wing Components for Civil Aircraft” Journal of the Royal Aeronautical Society November, 1952CrossRefGoogle Scholar
P R Payne “The stiff-hinged rotor” Aircraft Engineering Oct, 1955Google Scholar