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Small Turbofan Engines: Their impact on General Aviation Aircraft
ISSN: 0148-7191, e-ISSN: 2688-3627
Published April 01, 1981 by SAE International in United States
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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.
|Technical Paper||DESIGN FEATURES OF THE GARRETT ATF3 TURBOFAN ENGINE|
|Technical Paper||Military/Commercial Aircraft Propulsion Relationships|
CitationI'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.
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- Frost T.H. “Practical Bypass Mixing Systems for Fan Jet Aero Engines,” The Aeronautical Quarterly May 1966