Aerodynamic force coefficients were obtained for the model which has eight rectangular sails with symmetric uncambered NACA0018 section. A symmetric section was used so the airfoils may be used with the wind incident on either face. Tests were run with three types of sail set; with sails parallel, with trim angles graduated to attempt identical local flow conditions at all airfoils, and with trim angle reduced in equal steps of n degrees working from bow to stern. Runs were made at various inflow angles. Details of the aerodynamic interaction between sails are noted.


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    Titel :

    Wind Tunnel Tests of a Model Aerofoil Ship


    Beteiligte:

    Erscheinungsdatum :

    1980


    Format / Umfang :

    34 pages



    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Wind tunnel tests of aerofoil R.A.F. 36

    Bradfield, F. B. ;Clark, K. W. | SLUB | 1928