In the study of Buckling of uniform column under an axial load F, the deflection y(x) is obtained from the following equation with no deflections at x=0 and x=L:
@ganeshie8 can u help me
r u getting it sir
characteristic equation is \(\large r^2 + \gamma ^2 = 0\) right ?
is it very difficult sir because i tried for a long time but can't get it
u should start with making an auxiliary equation like \[D^2+\gamma^2=0\] \[D=(+-)i \gamma\] so the complementary function will be \[C.F=C_1\cos(\gamma x)+C_2\sin(\gamma x)\] like this
and what do u mean by first critical load?
if i do in that i am getting C sqrt(C^2+1)!=C^2+1 and x = (2 (tan^(-1)(C-sqrt(C^2+1))+pi n))/gamma and n element Z
i think here they want to covert to an differential equation n then solve but i don't rely know how to get a differential equation from this @sidsiddhartha
don't know to convert to differential equation sorry for the typing mistake
i think they only asked for the general solution and why u want to convert the diff equation?
i really don't it was a random guess and not good at differentials
i think all they want is the complementary function and that will be the general solution and,sorry i dont have any idea about the crictical load thing
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