Gas turbine requirements for V/STOL aircraft are strongly influenced by type of airplane and mission to be performed; gas turbine requirements are established in several propulsion-system concepts which encompass majority of engine requirements necessary to V/STOL airplanes; specific requirements for air superiority fighter airplane, subsonic fighter attack airplane, and transport-cargo type of airplane are discussed; these three types of airplanes use propulsion systems incorporating lift turbojet engines, turbofan engines, fans with remote gas generators, and turboprop engines.


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    Title :

    V/STOL aircraft gas turbine requirements


    Additional title:

    ASME -- Paper


    Contributors:

    Conference:

    ASME Meeting GT-48 ; 1967



    Publication date :

    1967


    Size :

    12 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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