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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
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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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, 0 = 26° ? Neglect the size of the airplane and the effect of lift caused by the wings during the motion Datum 30 m A
Transcribed Image Text: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, 0 = 26° ? Neglect the size of the airplane and the effect of lift caused by the wings during the motion Datum 30 m A
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