Predicated on the assumption of certain normal conditions for engine and propeller, simple expressions for the static and dynamic stresses of propeller blade roots are evolved. They, in combination with the fatigue strength diagram of the employed material, afford for each engine power one certain operating point by which the state of stress serving as a basis for the design of the root is defined. Different stress cases must be analyzed, depending on the vibration tendency of engine and use of propeller. The solution affords an insight into the possible introduction of different size classes of propeller.


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    Title :

    The design of propeller blade roots


    Contributors:
    Cordes, G (author)

    Publication date :

    1942-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



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