X-21A research aircraft is designed to demonstrate practicality of design, manufacture, operation, and maintenance of Laminar Flow Control aircraft and to acquire data for direct application to future aircraft systems; laminar flow control principle and concept of pumping system to remove boundary layer air from wing surfaces of Laminar Flow Control aircraft; pumping system requirements and design characteristics for future applications; system selection, and system operation; pumping design and development.


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    Title :

    Air pumping system for laminar flow control aircraft


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1963



    Publication date :

    1963


    Size :

    13 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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