Engineering formula
Resultant Bending Moment
$$Mb = √(Mx² + My²)$$
If mutually perpendicular bending-moment components $M_x$ and $M_y$ act simultaneously at a section, the magnitude of the resultant bending moment is:
$$M_b=\sqrt{M_x^2+M_y^2}.$$
For a circular section, whose geometric properties are identical about any centroidal axis in the section plane, the maximum bending normal stress can be calculated as:
$$|\sigma_b|=\frac{M_b}{W}.$$
- $M_x$, $M_y$ — bending-moment components;
- $M_b$ — resultant bending moment;
- $W$ — bending section modulus;
- $\sigma_b$ — bending normal stress.
For noncircular sections, the orientation of the bending moment and the second moments of area about the corresponding principal axes must generally be considered explicitly.