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Modern Propellers for Commuter Airlines
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English
Abstract
Modern airline propellers show significant improvements in weight, noise, cost and complexity over those designed in the 1950’s and 60’s and still in service. These improvements have come as the result of development work started a considerable number of years ago, covering aerodynamics, hub structure, blade retention, pitch control system and composite blades. These developments and associated design philosophies regarding safety and minimising maintenance costs are discussed, together with the achievement of the test background essential before new ideas can be introduced into service. In the near future wider blades and/or an increased number of blades are likely to be required as cruise speeds are pushed upwards and noise becomes an even more important design parameter.
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Citation
Russell, J., "Modern Propellers for Commuter Airlines," SAE Technical Paper 820719, 1982, https://doi.org/10.4271/820719.Also In
References
- Bocci, A. J. “A new series of aerofoil sections suitable for aircraft propellers.” Aeronautical Quarterly February 1977
- Rohrback C. Wainauski, B. S. “Aerodynamic Characteristics of an advanced technology propeller for Commuter aircraft.” Paper AIAA-81-1565 presented at AIAA/SAE/ASME 17th Joint Propulsion Conference, Colorado Springs July 1981
- Pearce, C. M. “Some propeller developments in the U.K.” Paper AIAA-81-1566 presented at AIAA/SAE/ASME 17th Joint Propulsion Conference, Colorado Springs July 1981
- Davis, D. G. M. “The Impact of Noise Regulations on Propeller Design.” SAE Paper 790593 presented at Business Aircraft Meeting and Exposition Century II , Wichita April 1979
- Jerachi R. J. Mitchell, G. A. “Low and high speed Propellers for General Aviation -Performance potential and recent wind tunnel test results.” NASA Technical Memorandum 81745. Prepared for the National Business Aircraft meeting sponsored by the SAE Wichita, Kansas April 1981
- Reed, E. G. “Studies of blade shank form and pitch distribution for constant speed propellers.” NACA 1945
- Maynard, J. D. “Aerodynamic characteristics at high speeds of full scale propellers having different shank designs.” NACA 1947
- Trebble, W. J. G. Williams J. Donnelly, R. P. “Comparative acoustic wind tunnel measurements and theoretical correlations on subsonic aircraft propellers at full scale and model scale.” R. A. E. Technical Memo Aero 1909 July 1981 AIAA-81-2004 and presented at the AIAA 7th Aero-acoustics Conference at Palo Alto California October 1981
- Colclough W. J. Russell, J. G. “The development of a composite propeller blade with a carbon fibre reinforced plastics spar.” The Aeronautical Journal January 1972
- Russell, J. G. “Use of reinforced plastics in a composite propeller blade.” Plastics and Polymers December 1973
- McCarthy, R. “Fifteen years experience with composite propeller blades.” Paper presented at European Chapter SAMPE International Conference on Advanced Technology in Materials Engineering, Cannes, France January 1981