The LANN wing is the result of a joint effort between Lockheed, the Air Force, NASA, and the Netherlands to measure unsteady pressures at transonic speeds. It is a moderate-aspect-ratio transport wing configuration. The wing was machined from NITRONIC 40 and has 12 percent thick supercritical airfoil sections.


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    Title :

    LANN wing design


    Contributors:


    Publication date :

    1983-03-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English







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