An airfoil design method has been developed which, with the aid of a mini-computer, can be used to determine the velocity distributions that will produce desired design parameters (lift, drag, and pitching moment) at the design condition and test for boundary layer separation. Use of a generalized equation for the velocity allows the design parameters to be determined as a function of coefficients of an integrated expression. Therefore, any series of general velocity distributions can be analyzed and the best one for the design mission selected.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    An Approach to Subsonic, Turbulent Flow Airfoil Design Using Mini-Computers


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1977



    Erscheinungsdatum :

    1977-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Kinematics of the Turbulent and Nonturbulent Interfaces in a Subsonic Airfoil Flow

    Zhang, Huiying / Rival, David E. / Wu, Xiaohua | AIAA | 2021



    Computation of Trailing Edge Noise of a 3D Lifting Airfoil in Turbulent Subsonic Flow

    Ewert, Roland / Meinke, Matthias / Schroeder, Wolfgang | AIAA | 2003


    Robust, Optimal Subsonic Airfoil Shapes

    Rai, Man Mohan | NTRS | 2014