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2.2 Squares, Cubes, and Roots

Key Takeaways

  • Squaring and cubing non-linear expressions are common when analyzing physical, thermodynamic, and electrical systems.

  • Circular Mil Area (CMA) is calculated as the square of the conductor diameter in mils, simplifying electrical cable calculations.

  • Kinetic energy scales quadratically with velocity, meaning that small speed increases require significantly more brake thermal capacity.

  • Root-Mean-Square (RMS) voltage represents the effective heating potential of AC electricity and relates to peak voltage by a factor of the square root of 2.

Last updated: July 2026

2.2 Squares, Cubes, and Roots

In aviation maintenance mathematics, you will frequently encounter quadratic and cubic relationships. Physical properties such as electrical resistance, kinetic energy, and alternating current parameters do not scale linearly. This section covers the calculations of squares, cubes, square roots, and cube roots, and details their essential applications in aircraft systems.

Squares and Cubes

  • Squaring a number means multiplying the number by itself. It is represented as x2x^2.
  • Cubing a number means multiplying the number by itself twice (three factors of the number). It is represented as x3x^3.

In EASA exams, you will often need to calculate these values without the aid of a calculator. Let's review key arithmetic properties, particularly involving fractions and decimals:

  1. Decimals: When squaring a decimal, the number of decimal places in the result is twice the number of decimal places in the original number. For example, (0.05)2=0.05×0.05=0.0025(0.05)^2 = 0.05 \times 0.05 = 0.0025 (two decimal places in the base become four in the result). For cubing, it is three times: (0.2)3=0.2×0.2×0.2=0.008(0.2)^3 = 0.2 \times 0.2 \times 0.2 = 0.008 (one decimal place becomes three).
  2. Fractions: To square or cube a fraction, square or cube the numerator and denominator independently: (34)2=3242=916\left(\frac{3}{4}\right)^2 = \frac{3^2}{4^2} = \frac{9}{16} (23)3=2333=827\left(\frac{2}{3}\right)^3 = \frac{2^3}{3^3} = \frac{8}{27}

Square Roots and Cube Roots

  • The square root of a number xx, denoted as x\sqrt{x} or x1/2x^{1/2}, is a value that, when multiplied by itself, equals xx.
  • The cube root of a number xx, denoted as x3\sqrt[3]{x} or x1/3x^{1/3}, is a value that, when multiplied by itself twice, equals xx.

Manual Estimation Technique for Roots

When calculators are not permitted, finding roots of non-perfect squares requires estimation or prime factorization.

  • Estimation Method: To find 55\sqrt{55}, identify the nearest perfect squares: 72=497^2 = 49 and 82=648^2 = 64. Since 5555 is between 4949 and 6464, its square root is between 77 and 88. A linear interpolation suggests 55≈7.4\sqrt{55} \approx 7.4.
  • Fractions and Decimals: 0.09=0.3(since 0.3×0.3=0.09)\sqrt{0.09} = 0.3 \quad (\text{since } 0.3 \times 0.3 = 0.09) 1625=1625=45=0.8\sqrt{\frac{16}{25}} = \frac{\sqrt{16}}{\sqrt{25}} = \frac{4}{5} = 0.8 0.0083=0.2(since 0.2×0.2×0.2=0.008)\sqrt[3]{0.008} = 0.2 \quad (\text{since } 0.2 \times 0.2 \times 0.2 = 0.008)

Aviation Application: Circular Mil Area (CMA)

In aircraft electrical maintenance, wire sizes are defined by their cross-sectional area. Standard commercial aircraft contain miles of wiring, and selecting the correct gauge is critical to prevent overheating and voltage drop.

Instead of measuring wire area in square inches or square millimeters (which requires multiplying by π\pi), the aviation industry utilizes the circular mil (cmil).

  • Mil: A unit of length equal to 0.001 inches0.001\text{ inches} (10−3 in10^{-3}\text{ in}).
  • Circular Mil: The area of a circle with a diameter of 1 mil1\text{ mil}.

The formula to calculate the Circular Mil Area (CMA) of a conductor is:

CMA=d2\text{CMA} = d^2

Where dd is the diameter of the conductor expressed in mils.

Worked Example: Calculating Wire CMA

An aircraft technician is replacing a generator power feeder cable. The manual specifies a conductor diameter of 0.080 inches0.080\text{ inches}. What is its area in circular mils, and what would the diameter be if the CMA was 10,000 circular mils10,000\text{ circular mils}?

  1. Convert Diameter to Mils: d=0.080 in×1000 mils/in=80 milsd = 0.080\text{ in} \times 1000\text{ mils/in} = 80\text{ mils}
  2. Calculate CMA: CMA=d2=802=6400 circular mils\text{CMA} = d^2 = 80^2 = 6400\text{ circular mils}
  3. Find Diameter from a Given CMA of 10,000: d=CMA=10000=100 milsd = \sqrt{\text{CMA}} = \sqrt{10000} = 100\text{ mils} Diameter in inches=100 mils×0.001 in/mil=0.100 inches\text{Diameter in inches} = 100\text{ mils} \times 0.001\text{ in/mil} = 0.100\text{ inches}

Using circular mils simplifies calculations for engineers, as resistance per unit length is directly inversely proportional to the CMA. Additionally, circular mils and square mils are related as follows: 1 circular mil=π4 square mils≈0.7854 square mils1\text{ circular mil} = \frac{\pi}{4}\text{ square mils} \approx 0.7854\text{ square mils}.


Aviation Application: Kinetic Energy (Ek=12mv2E_k = \frac{1}{2}m v^2)

During aircraft landing operations or a rejected takeoff (RTO), the aircraft's kinetic energy must be completely absorbed and dissipated as heat by the wheel brakes. Kinetic energy (EkE_k) is governed by the formula:

Ek=12mv2E_k = \frac{1}{2}m v^2

Where:

  • mm is the mass of the aircraft (in kg).
  • vv is the velocity of the aircraft (in m/s).

Because velocity is squared, the kinetic energy scales quadratically with speed. This means a minor increase in speed results in a disproportionately large increase in kinetic energy, which can exceed the thermal limits of the brakes and cause brake fires or tire blowouts.

Worked Example: Brake Energy Scaling

An aircraft with a landing mass of 12,000 kg12,000\text{ kg} is landing at a speed of 45 m/s45\text{ m/s} (approx. 87 knots87\text{ knots}).

  1. Calculate the baseline Kinetic Energy:

    Ek=0.5×12000 kg×(45 m/s)2=6000×2025=12,150,000 Joules=12.15 MJE_k = 0.5 \times 12000\text{ kg} \times (45\text{ m/s})^2 = 6000 \times 2025 = 12,150,000\text{ Joules} = 12.15\text{ MJ}
  2. Calculate Energy if landing speed increases to 60 m/s60\text{ m/s} (due to tailwind or flap failure):

    Ek=0.5×12000 kg×(60 m/s)2=6000×3600=21,600,000 Joules=21.60 MJE_k = 0.5 \times 12000\text{ kg} \times (60\text{ m/s})^2 = 6000 \times 3600 = 21,600,000\text{ Joules} = 21.60\text{ MJ}

Although the speed increased by only 33.3%33.3\% (from 45 to 60 m/s45\text{ to } 60\text{ m/s}), the kinetic energy that the brakes must dissipate increased by 77.8%77.8\% (from 12.15 to 21.60 MJ12.15\text{ to } 21.60\text{ MJ}). This highlights the mathematical danger of high-speed landings.


Aviation Application: Root-Mean-Square (RMS) Voltage

Commercial aircraft electrical systems typically use 115 V115\text{ V} Alternating Current (AC) at a frequency of 400 Hz400\text{ Hz}. The voltage of an AC system varies as a sine wave over time. The nominal value of 115 V115\text{ V} is not the peak voltage, but rather the Root-Mean-Square (RMS) value.

RMS represents the equivalent Direct Current (DC) voltage that would deliver the same electrical power (heating effect) to a resistive load. To calculate RMS mathematically:

  1. Square the values of the sine wave.
  2. Find the Mean of these squared values.
  3. Take the Square Root of the mean.

For a sinusoidal AC voltage, the relationships between RMS voltage (VrmsV_{rms}) and Peak voltage (VpeakV_{peak}) are:

Vrms=Vpeak2≈0.707×VpeakV_{rms} = \frac{V_{peak}}{\sqrt{2}} \approx 0.707 \times V_{peak} Vpeak=Vrms×2≈1.414×VrmsV_{peak} = V_{rms} \times \sqrt{2} \approx 1.414 \times V_{rms}

Worked Example: Insulation Voltage Rating

An avionics technician needs to select wire insulation for a 115 V115\text{ V} AC bus. The insulation must withstand the peak voltage of the system without breaking down. What is the peak voltage of the 115 V115\text{ V} AC system?

Vpeak=115 V×2≈115×1.4142≈162.63 VV_{peak} = 115\text{ V} \times \sqrt{2} \approx 115 \times 1.4142 \approx 162.63\text{ V}

The wire insulation must be rated to handle at least 163 V163\text{ V} of electrical potential, even though the nominal system voltage is only 115 V115\text{ V}.

Test Your Knowledge

An aircraft electrical conductor has a diameter of 0.050 inches. What is its cross-sectional area in circular mils (CMA)?

A

1,963 circular mils

B

2,500 circular mils

C

5,000 circular mils

D

0.0025 circular mils

Test Your Knowledge

If the landing speed of a 10,000 kg aircraft is increased from 50 m/s to 100 m/s, how does the kinetic energy that must be dissipated by the landing gear brakes change?

A

It increases by a factor of 2, from 12.5 MJ to 25 MJ

B

It increases by a factor of 1.414, from 12.5 MJ to 17.7 MJ

C

It increases by a factor of 4, from 12.5 MJ to 50 MJ

D

It increases by a factor of 8, from 12.5 MJ to 100 MJ

Test Your Knowledge

The AC electrical system of a commercial aircraft operates at a nominal value of 115V RMS. What is the peak voltage (V_peak) experienced by the system's insulation?

A

81.3V

B

115.0V

C

141.4V

D

162.6V

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