The design procedure of a basic airfoil for a slightly swept transport aircraft wing is described. It is shown that transonic wing technology reduces sweep by retaining wing thickness and cruise Mach number.


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    Title :

    Design of a Basic Airfoil for a Slightly Swept Wing. Part 1: Theoretical Transonic Airfoil Design


    Contributors:
    G. Wichmann (author)

    Publication date :

    1984


    Size :

    47 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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