Hi friends,
How to find moment of inertia and natural frequency of a trapezoidal plate having thickness 6mm and it looks like aircraft wing.
please help me to solve this problem
Ya what u said is right but that is general ..but i want specific to cantilever beam.As u said strain equals to stress by young's modulus.Where stress equals to force by area.can u send some document regarding to my mail id if so my id is zoom143.ashwin@gmail.com...
I am not cleared with wat u have given answer about how to find strain. Can u just send me formula to find strain of cantilever beam of rectangular cross section having point load at its free end with description of formula.
Hello to everyone,
my question is how to find strain in rectangular cantilever beam applying point load at some point. I am not getting formulas for that..Please save me from this. Its very urgent for me.