Answer to Question #147099 in Mechanical Engineering for Windia paklungang

Question #147099
One of the tail rotor blades of a helicopter has an unbalanced mass of m 0.5 kg at a distance of e=0.15 m from the axis of rotation as shown below. The tail boom has a length of 4 m, a mass of 240 kg, a flexural stiffness EI of 2.5 × 10^6 N-m^2 and a damping ratio of 0.15. The mass of the tail rotor blades. including their drive system, is 20 kg. Determine the forced response of the tail boom (displacement at the tail rotor shaft) when the blades rotate at 1500 RPM. Assume that the tail boom has uniform properties along its length. Tail rotor blades Tail section. El
1
Expert's answer
2020-12-07T03:41:24-0500
Dear Windia paklungang, your question requires a lot of work, which neither of our experts is ready to perform for free. We advise you to convert it to a fully qualified order and we will try to help you. Please click the link below to proceed: Submit order

Need a fast expert's response?

Submit order

and get a quick answer at the best price

for any assignment or question with DETAILED EXPLANATIONS!

Comments

No comments. Be the first!

Leave a comment

LATEST TUTORIALS
New on Blog
APPROVED BY CLIENTS