This paper describes the design and operation of the pumping system used to remove boundary layer air from the wing surfaces of the X-21A Laminar Flow Control airplanes. Included are comments on pumping system requirements and design characteristics for future applications. Part 1 includes a discussion of the initial problem statement, system selection, and system operation. Part 2 covers the pumping design and development.


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    Titel :

    Air Pumping System for a Laminar Flow Control Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Getz, D. L. (Autor:in) / Wallace, F. B. (Autor:in) / Monahan, W. A. (Autor:in) / Collins, W. L. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1963




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Air pumping system for laminar flow control aircraft

    Collins, W.L. / Monahan, Jr., W.A. / Getz, D.L. et al. | Engineering Index Backfile | 1963


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    R. D. Joslin | NTIS | 2004


    Aircraft Laminar Flow Control

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    Laminar Flow Aircraft Certification

    L. J. Williams | NTIS | 1986


    Laminar Flow Aircraft Certification

    Williams, Louis J. | NTRS | 1986