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  • Mechanical Engineering  (1)
  • 1940-1944  (1)
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    Publication Date: 2019-07-11
    Description: The exact mathematical treatment of the problem is possible by replacing the propeller blade by a homogeneous prismatic rod. Conclusions can them be drawn as to the behavior of an actual propeller, since tests on propeller blades have indicated a qualitative agreement with the homogeneous rod. The natural frequencies are determined and the stressing of the systems under the various vibration modes are discussed.
    Keywords: Mechanical Engineering
    Type: NACA-TM-1051 , Jahrbuch 1938 der Deutschen Luftfahrtforschung; 141-159
    Format: application/pdf
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