A propeller with tip radius of 1.2m is rotating at 1200rpm. If the propeller tip blade...

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A propeller with tip radius of 1.2m is rotating at 1200rpm. If the propeller tip blade angle (propeller blade chord to disk of rotation angle) is at 35.7 degrees, calculate the maximum speed of the aircraft that would still allow the propeller tip to produce thrust. CL = 0.1(a + 5deg)deg- Provide your answer in m/s. A propeller with tip radius of 1.2m is rotating at 1200rpm. If the propeller tip blade angle (propeller blade chord to disk of rotation angle) is at 35.7 degrees, calculate the maximum speed of the aircraft that would still allow the propeller tip to produce thrust. CL = 0.1(a + 5deg)deg- Provide your answer in m/s.

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The problem youre asking about involves finding the maximum speed of an aircraft at which the propeller tip is still effective in generating thrust Th... View the full answer