Shell Aviation News n 254 Aug 1959 p 14-18. Technical considerations involved in determination of 250-hp engine design, developed by General Motors for small helicopters and light military aircraft; unique features are reviewed such as free turbine, selection of engine pressure ratio and turbine inlet temperature, engine air flow, matching of components, selection of compressor configuration, control system, and mechanical configuration. (See also SAE -- Paper n 49R for meeting Mar 31-Apr 3 1959 26 p)


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    Title :

    Design approach to Allison model 250 engine


    Additional title:

    SAE -- J


    Contributors:
    Hall, R.S. (author)


    Publication date :

    1959


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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