Thrust losses due to shanks were of order of 9% at airplane Mach number of 0.7 when propeller was operating at highest test power coefficient of 0.17per blade; loss in thrust due to shanks was function primarily of airplane Mach number and was relatively independent of blade loading.


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    Titel :

    Investigation of thrust losses due to shanks of flared-shank two-blade propeller on slender-nose airplane


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Hammack, J.B. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    6 pages


    Anmerkungen:

    8 Supp Sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Airplane propeller thrust

    Rauch, C.W. | Engineering Index Backfile | 1928


    Measurement of propeller blade shank

    Cordes, G. | Engineering Index Backfile | 1941


    Shovel blade airplane/boat propeller

    KIPNIS MICHAEL | Europäisches Patentamt | 2024

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