The gantry structure in the photo is used to test the response of an airplane during a crash. As shown below., the plane, having amass of 4.43 Mg, is hoisted back until 0 = 71°, and then the pull-back cable AC is released when the plane is at rest. What is the maximum tension (kN) developed in the supporting cable just before the airplane crashes into the ground, e = 26° ? Neglect the size of the airplane and the effect of lift caused by the wings during the motion Datum 30 m

The gantry structure in the photo is used to test the response of an airplane during a crash. As shown below., the plane, having amass of 4.43 Mg, is hoisted back until 0 = 71°, and then the pull-back cable AC is released when the plane is at rest. What is the maximum tension (kN) developed in the supporting cable just before the airplane crashes into the ground, e = 26° ? Neglect the size of the airplane and the effect of lift caused by the wings during the motion Datum 30 m

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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