In an airframe assembly,whats the use of STRESS ANALYSIS
being conducted on newly designed component or modified
component...?
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Answer Posted / nav
Reason for STRESS ANALYSIS being conducted on newly
designed component or modified component is
1.To check the reliability of the structure/component or
part that has been fixed new over the load spectrum.This is
further done by calculating the MS(margin of safety =
(Allowable/Applied)-1)).
2.It helps in calculating the strength of a structure and
optimise to the requirement, which can help in weight
saving.(which is vey imp in aircraft industry).
3.It also helps engineer to understand the behavoiur of the
structure in various nature(tension, compressive) of the
load.
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