Semester : SEMESTER 4
Subject : Aircraft Structures-I
Year : 2020
Term : SEPTEMBER
Branch : AERONAUTICAL ENGINEERING
Scheme : 2015 Full Time
Course Code : AO 204
Page:4
020004 0204052001
1 |
Cylinder h
1. Determine the impact factor.
11. | Determine the maximum shortening of the spring due to the impact
14 a) A circular rod of length L and cross section area A is attached to spring having 5
stiffness K as shown in the figure.
Let 8 is the young’s modulus and © be the coefficient of thermal expansion of the
rod. If the bar subjected to temperature increase of AT, determine the expression
for thermal stress developed on the cross section.
b) What is endurance limit? Explain the failure mechanism of components under 5
fatigue loading.
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