Wing sections with laminar flow and their effects on fuel consumption are discussed. It was shown that laminarization by section shape is possible at certain Reynolds numbers and at reduced Mach numbers.


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    Title :

    Laminar-Airfoils for Transport Aircraft


    Contributors:
    A. Quast (author)

    Publication date :

    1980


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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