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B Rotation of the blades of a jet engine

  1. Feb 4, 2017 #1
    Hi im Maximilian I'm working on a schoolproject
    The mechanical part of the jet engine and i wanted to calculate the normal acceleration of a blade of the turbine and i got u huge number. 211680 m/s² and 1437043 m/s². for a rpm of 4012 and 10450rmp so thats w = 420 rad/s and 1094 rad/s and the blade is 120 cm
    ty for the help in the word document you can see how i came to the numbers i marked it in yellow
    Maximilian
     

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  2. jcsd
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