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Aerodynamic Aspects of Helicopter Design

Published online by Cambridge University Press:  26 October 2023

H Roberts

Extract

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The CHAIRMAN, in introducing the Author, said that Dr ROBERTS was very well known by everybody in the helicopter field m this country and abroad He had taken his B Sc Engineering Degree at Queen Mary College and his Ph D at Imperial College He had served with General Aircraft Ltd, and had also been a lecturer at Imperial College Subsequent to this appointment he had been with Saunders-Roe as Chief Project Engineer (Helicopters), and was now on the staff of Fairey Aviation where initially he had been Chief Aerodynamicist and was now Chief Project Engineer Dr Roberts was a Founder Member and a member of the Council of the Association

Type
Research Article
Information
The Journal of the Helicopter Association of Great Britain , Volume 10 , Issue 1 , July 1956 , pp. 24 - 60
Copyright
Copyright © Royal Aeronautical Society 1956

References

1 Aerodynamic Design of Helicopters Wood, K D Inst of Aero Sciences PreprintGoogle Scholar
2 Some Aerodynamic Problems of the Helicopter Squire, H B Journal of the Helicopter Assoc Gt Britain Vol 1, No 3Google Scholar
3 Some Aerodynamic Aspects of Rotor Blade Design Squire, H B Journal of the Helicopter Assoc Gt Britain Vol 5, No 3Google Scholar
4 Some Major Problems in Helicopter Aerodynamics Hislop, G S Paper read at the 6th meeting of the A G A R D Flight Test Panel Nov /Dec, 1954Google Scholar
5 Introduction to Helicopter Aerodynamics Vol 1 Performance Stepniewski, W Z (Rotorcraft Publishing Committee)Google Scholar
6 Helicopter Analysis Nikolsky, A A (John Wiley)Google Scholar
7 Contribution to the Aerodynamics of Rotary Wing Aircraft Sissingh, G NACA Technical Memorandum 921, 1929Google Scholar
8 The Effect of Planform on Static Thrust Performance Q Wald Sikorsky Aircraft S E R 442, Nov, 1944Google Scholar
9 Aerodynamics of the Hehcopter Gessow, A and Myers, G C (Macmillan, New York, 1952)Google Scholar
10 Review of Information on Induced Flow of a Lifting Rotor Gessow, A NACA Technical Note 3238Google Scholar
11 The Low Speed Performance of a Helicopter Oliver, A L Current Paper No 122Google Scholar
12 The Normal Component of the Induced Velocity in the Vicinity of a Lifting Rotor and some Examples of its Application Castles, W and DeLeeuw, J H NACA Report 1184Google Scholar
13 Some Observations of Surface Contamination on Helicopter Rotor Blades Gregory, J D L Unpublished A R C Report, July, 1955Google Scholar
14 Induced Aerodynamics of Helicopters, Part II Payne, P R Aircraft Engineering, March, 1956Google Scholar
15 An Analysis of N A C A Helicopter Reports Liptrot, R N S & T Memo No 7/54Google Scholar
16 Charts for Estimating Performance of High Performance Helicopters Gessow, A and Tapscott, R J N A C A Technical Note 3323, Jan, 1955Google Scholar
17 An Analysis of the Longitudinal Stability and Control of a Single Rotor Helicopter O’Hara, F Unpublished M O S ReportGoogle Scholar
18 A General Theory of Helicopter Rotor Dynamics Payne, P R Aircraft Engineering, August, 1954Google Scholar
19 The Disturbed Motion of Articulated Blades Roberts, H Unpublished A R C Report October, 1949Google Scholar
20 A Method of Improving the Inherent Stability and Control Characteristics of Helicopters Miller, R H Journal of the Aeronautical Sciences, June, 1950Google Scholar
21 The Effect of Viscous and Elastic Control System Restraints on Helicopter Stability and Control in Forward Flight McCabe, W L and McCaskill, A M Princeton University Aeronautical Engineering Laboratory Report No 281 August, 1954Google Scholar