Scroll back to top
Taken from TAM251 Lecture Notes - L13S2
Taken from TAM251 Lecture Notes - L13S3
Taken from TAM251 Lecture Notes - L13S4
Taken from TAM251 Lecture Notes - L13S5
**Expandable Derivation**
**End Derivation**
Euler's formula can be used to solve for the critical load of a uniaxially loaded column.
Taken from TAM251 Lecture Notes - L13S6
**Expandable Derivation**
Buckling usually happens at the smallest non-zero value of \( P_{cr} \)
Higher \( n \) values can be achieved if columns are prevented from buckling at \( n=1 \)
**End Derivation**
Taken from TAM251 Lecture Notes - L13S8
Different boundary conditions change length used in the critical load formula to the effective length (\( L_e \)).