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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    6 pages


    Remarks:

    8 Supp Sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English






    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 | European Patent Office | 2024

    Free access