נפחים של גופי סיבוב

The disk method divides a solid of revolution into infinitesimally thin circular disks perpendicular to the axis of rotation. Each disk's area equals π times the square of the function's radius value. By integrating these disk areas over the specified interval, you accumulate the total volume of the solid using calculation of volume of solids by integration.

A fuel tank is modeled by rotating a two-dimensional region defined by a mathematical function about the x-axis. The region extends from zero to two meters along the axis, creating a three-dimensional symmetric shape. This approach allows engineers to calculate precise fuel capacity and weight distribution for aircraft performance.

First, square the function defining the tank's boundary to get the disk area formula. Then expand the resulting expression to identify terms with third and fourth powers of the variable. Finally, integrate these terms over the interval from zero to two meters and evaluate the definite integral by substituting the limits.

The disk method is appropriate because the boundary curve lies directly against the axis of rotation, creating circular cross-sections perpendicular to the x-axis. This geometry allows each disk's radius to equal the function value at that position, making the method straightforward and accurate for calculating the tank's volume.

The antiderivative describes how volume accumulates along the axis of integration as you move from zero to two meters. It captures the cumulative effect of all infinitesimal disk areas stacked along the tank's length. Evaluating this antiderivative at the limits yields the total internal capacity of approximately one cubic meter.

The definite integral evaluates the antiderivative at the upper limit of two meters and subtracts its value at the lower limit of zero. This calculation yields a numerical result that simplifies to approximately one cubic meter, representing the total fuel tank capacity needed for aerospace engineering applications.

Accurate volume estimates determine fuel capacity, weight distribution, and overall aircraft performance. Engineers must know exact tank dimensions to optimize fuel storage, balance aircraft weight, and ensure safe flight operations. Mathematical modeling through integration provides the precision necessary for reliable aerospace design and safety.