Worked, unit-aware calculation worksheets across structural, mechanical, electrical and more. Open any example into your own workspace to edit and reuse. New to Calculeaf? Start with your first worksheet or the examples guide.
515 examples
The number of cycles to fatigue failure predicted from an applied stress amplitude using the power-law form of the material's S-N curve.
The cumulative fatigue damage fraction from two distinct cyclic load levels, using the linear damage summation of Miner's rule.
The impact toughness of a material derived from Charpy V-notch test energy absorption normalized by the fractured ligament area.
The longitudinal elastic modulus of a fiber-reinforced composite predicted from the fiber and matrix moduli and the fiber volume fraction.
An empirical estimate of ultimate tensile strength from a measured Brinell hardness number, widely used for quick steel strength screening.
The shear stress on the effective throat of a fillet weld carrying a transverse or longitudinal load, the standard weld strength check.
The steady-state (secondary) creep strain rate of a material under sustained stress and elevated temperature, from the empirical Norton power law.
The number of cycles to failure under low-cycle (plastic-strain-dominated) fatigue loading, from the Coffin-Manson strain-life relation.
The recoverable elastic energy stored per unit volume in a material under uniaxial stress, a key quantity in resilience and impact-resistance comparisons.
An aircraft's still-air cruise range predicted from cruise speed, engine specific fuel consumption, aerodynamic efficiency, and the ratio of start-of-cruise to end-of-cruise weight.
An aircraft's steady rate of climb computed from the power available in excess of what is needed for level flight, divided by aircraft weight.
A turbojet engine's thrust computed from the momentum change it imparts to the air passing through it, neglecting pressure and fuel mass-flow terms.
A rocket engine's specific impulse computed from thrust, propellant mass flow rate, and standard gravity — the standard measure of propulsion efficiency.
The orbital period of a satellite in a circular orbit, computed from the orbit radius and the gravitational parameter of the central body.
The velocity change required for the first of two burns in a Hohmann transfer, the fuel-optimal way to move a spacecraft between two circular orbits.
An aircraft's load factor (structural g-loading) during a coordinated, constant-altitude turn as a function of bank angle.
The maximum structural load factor an aircraft can generate aerodynamically at its never-exceed speed, using maximum lift coefficient and wing area.
The static (zero-forward-speed) thrust of a propeller predicted from actuator disk (momentum) theory, given disk area and induced velocity.
The stagnation-to-static pressure ratio at which flow through a converging nozzle first reaches sonic velocity (Mach 1) at the throat.
Sample mean and sample standard deviation of five measured values, computed from first principles.
Converts a raw measurement into standard deviations from the mean (a z-score) for comparison against a normal distribution.
Best-fit straight line through four data points using the ordinary least-squares normal equations.
Minimum survey sample size needed to achieve a specified margin of error at a given confidence level.
Number of ordered arrangements (permutations) and unordered selections (combinations) of r items chosen from n.