Correction factors for ideal angle of attack and camber due to loading are presented for 3 Bladed 0.2R hub propellers.

    The factors are based on propeller lifting surface theory. Correction factors for ideal angle of attack due to thickness are not included. The propellers are optimum free-running propellers with chordwise loadings identical to NACA a = 0.8 meanline.


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    Titel :

    Lifting surface corrections for 3 bladed optimum propellers


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1971-12-01


    Format / Umfang :

    16 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Schlagwörter :


    Five-bladed propellers

    Slocum, S.E. | Engineering Index Backfile | 1950


    Chart for diameters of 3-bladed propellers

    Engineering Index Backfile | 1919


    Design diagrams of three-bladed controllable pitch propellers

    Tsuchida, Kiyoshi / Yazaki, Atsuo | TIBKAT | 1963


    Model tests on four-bladed controllable-pitch propellers

    Yazaki, A. | Engineering Index Backfile | 1964


    Further model tests on four-bladed controllable-pitch propellers

    Yazaki, Atsuo / Sugai, Nobuo | TIBKAT | 1966