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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
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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Physics
Authors: David Young, Shane Stadler
10th edition
1118486897, 978-1118836873, 1118836871, 978-1118899205, 1118899202, 978-1118486894
