Helicopter rotor has four blades

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    Helicopter Rotor
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The discussion focuses on calculating the linear speed of a helicopter rotor blade with a length of 3.90 meters and a rotational speed of 480 revolutions per minute. The correct formula to determine the linear speed is V = 2πR/T, where R is the blade length and T is the rotational speed. The calculations show that the distance traveled by the blade tip in one rotation is 24.5 meters, leading to a linear speed of 11760 meters per minute when factoring in the rotational speed. There is a consensus that the initial answer provided was incorrect, confirming the proper calculation method. Understanding these calculations is crucial for accurate aerodynamic assessments in wind tunnel experiments.
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A model of a helicopter rotor has four blades, each of length 3.90m from the central shaft to the blade tip. The model is rotated in a wind tunnel at a rotational speed of 480rev/min .

A.) What is the linear speed of the blade tip?

given
R= 3.9
T = 480

would it just be V= 2*pi*R/t
and got = .05105

someone helped me(not at this forum) and the answer is wrong. can someone help? isn't it just asking for the velocity?
 
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Well you say the rotational velocity is 480 rotations / minute
1 rotation at a distance R from the center is the cirumference of a circle, so the distance the tip travels in one rotation is : 2*Pi*Radius meters

D = 2*3.14159*3.90 = 24.5 meters

You say 480 Rot/Min => 480 (rotrotations/minute) * (24.5 meters/rotation) = 11760 meters per minute.
 


Yes, you are correct. The linear speed of the blade tip can be calculated using the formula V = 2πR/T, where V is the linear speed, R is the length of the blade, and T is the rotational speed in revolutions per minute (rev/min). Plugging in the given values, we get V = 2π(3.9)/480 = 0.05105 m/s. It is possible that the answer you were given is incorrect.
 
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