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Small Turbofan Engines: Their impact on General Aviation Aircraft
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English
Abstract
An evaluation is made on the application of small turbofan engines to general aviation aircraft. The influence of engine cycle parameters, such as bypass ratio and fan pressure ratio and other design features as related to mission and aircraft requirements, are presented.
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Authors
Citation
I'Anson, L. and Schneider, W., "Small Turbofan Engines: Their impact on General Aviation Aircraft," SAE Technical Paper 810622, 1981, https://doi.org/10.4271/810622.Also In
References
- Sievers G.K. et al “General Aviation Propulsion,” NASA Conference Publication 2126 November 28 1979
- Moellmann H.F. Schwaar P. W. “Small Turbine Engine Analysis and Preliminary Design,” Final Report to Air Force Aeropropulsion Laboratory, Technical Report AFAPL-TR-71-77 December 1971
- Frost T.H. “Practical Bypass Mixing Systems for Fan Jet Aero Engines,” The Aeronautical Quarterly May 1966