Two circulation control cambered elliptic airfoil sections with a thickness-to-chord ratio of 0.15- and 1.0-percent circular arc camber were evaluated subsonically to determine their aerodynamic characteristics. The two models, designated NCCR 1510-7067N and NCCR 1510-7567S, have a common leading edge but different Coanda surfaces.


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    Title :

    Two-Dimensional Subsonic Wind Tunnel Evaluation of Two Related Cambered 15-Percent Thick Circulation Control Airfoils


    Contributors:
    J. Abramson (author)

    Publication date :

    1977


    Size :

    68 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English