In physics and engineering, understanding the moments of inertia for a given area with asymmetrical mass distribution is critical for proper design and analysis. When considering an arbitrary coordinate system, the moments of inertia can be obtained by integrating the moment of inertia for an infinitesimal area element.

Suppose another coordinate system inclined at an angle is considered. In that case, the transformation relations can be used to express the moments and product of inertia along the inclined axes in terms of the inclined coordinates and area element.

By reducing the moments of inertia to a function of the initial coordinates and using trigonometric identities, the moment of inertia along the inclined axes can be obtained.

Similarly, the transformation relations are applied in the expression for the product of inertia to calculate the product of inertia along the inclined axes.

When the moment of inertia along the original axes is added, the polar moment of inertia along the z-axis is obtained that is independent of the orientation of the inclined axes.

The moments of inertia and product of inertia along the inclined axes are essential in designing various structures, such as aircraft wings, to determine their stiffness. By understanding the moments of inertia and the product of inertia along different axes, engineers and designers can determine how various forces and loads will affect the structure, providing vital information for safe and effective design.