6-26. The loading on a control torque tube for an aileron of an airplane may be idealized by a uniformly varying torque Tx = kx in-Ib/in, where k is a constant(see the figure). Determine the angle of twist of the free end. Assume IpG to be constant. Fig. P6-26
6-26. The loading on a control torque tube for an aileron of an airplane may be idealized by a uniformly varying torque Tx = kx in-Ib/in, where k is a constant(see the figure). Determine the angle of twist of the free end. Assume IpG to be constant. Fig. P6-26
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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6-26. The loading on a control torque tube for an aileron of an airplane may be idealized by a uniformly varying torque Tx = kx in-lb/in, where k is a constant(see the figure). Determine the angle of twist of the free end. Assume IpG to be constant.
![6-26. The loading on a control torque tube for an aileron of an airplane may be
idealized by a uniformly varying torque Tx = kx in-Ib/in, where k is a constant(see
the figure). Determine the angle of twist of the free end. Assume IpG to be constant.
Fig. P6-26](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F7f0069ce-7c3f-43d4-9141-588239e37101%2F95bc801d-8246-4cdc-aedb-34254faedb28%2Fos4p8o6f_processed.png&w=3840&q=75)
Transcribed Image Text:6-26. The loading on a control torque tube for an aileron of an airplane may be
idealized by a uniformly varying torque Tx = kx in-Ib/in, where k is a constant(see
the figure). Determine the angle of twist of the free end. Assume IpG to be constant.
Fig. P6-26
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