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.


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    Title :

    Pressure distribution over airfoils with fowler flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1938


    Size :

    19 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    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


    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


    Lift Augmentation on Hollow Airfoils with Flaps

    Yeung, W. W. H. / Goh, E. K. / Jiang, Y. T. et al. | British Library Conference Proceedings | 2001