The design was based on the LTS-101 engine family for the core engine. A high bypass fan design (BPR=9.4) was incorporated to provide reduced fuel consumption for the design mission. All acoustic and pollutant emissions goals were achieved. A discussion of the preliminary design of a business jet suitable for the developed propulsion system is included. It is concluded that large engine technology can be successfully applied to small turbofans, and noise or pollutant levels need not be constraints for the design of future small general aviation turbofan engines.


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    Title :

    Design and Evaluation of an Integrated Quiet, Clean General Aviation Turbofan (QCGAT) Engine and Aircraft Propulsion System


    Contributors:
    J. German (author) / P. Fogel (author) / C. Wilson (author)

    Publication date :

    1980


    Size :

    226 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English