Tests made on Clark Y airfoil with 0.20cw Clark Y Fowler flap and on N ACA 23012 airfoil with 0.20cw, 0.30cw, 0.40cw NACA 23012 Fowler flaps; test installation was used in which model was mounted in wind tunnel between large end planes so that two-dimensional flow was approximated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Pressure distribution over airfoils with fowler flaps


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Wenzinger, C.J. (Autor:in) / Anderson, W.B. (Autor:in)


    Erscheinungsdatum :

    1938


    Format / Umfang :

    19 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Pressure distribution over airfoils with fowler flaps

    Wenzinger, C.J. / Anderson, W.B. | Engineering Index Backfile | 1938


    Pressure distribution over airfoils with Fowler flaps

    Wenzinger, Carl J. / Anderson, Walter B. | TIBKAT | 1938


    Pressure distribution over airfoils with fowler flaps

    Wenzinger, C.J. / Anderson, W.B. | Engineering Index Backfile | 1938


    THE PRACTICAL APPLICATION OF FOWLER FLAPS

    FOWLER, HARLAN D. | SAE Technical Papers | 1937


    Design Philosophies for Sailplane Airfoils with Flaps

    Eppler, R. / Wurz, W. | British Library Online Contents | 2000