Maximum-lift coefficient of airplane, based on original wing area, was increased from 1.35 to 1.96 while minimum drag was increased from 0.050 to 0.052; landing speed decreased 9 mph; level-flight speed increased 10%.


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    Title :

    Flight tests to determine effect of fixed auxiliary airfoil on lift and drag of parasol monoplane


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Soule, H.A. (author)


    Publication date :

    1932


    Size :

    9 pages


    Remarks:

    9 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :