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The Wilks coefficient or Wilks formula is a mathematical coefficient that can be used to measure the relative strengths of powerlifters despite the different weight classes of the lifters. Robert Wilks, CEO of Powerlifting Australia , is the author of the formula.
The capstan equation [1] or belt friction equation, also known as Euler–Eytelwein formula [2] (after Leonhard Euler and Johann Albert Eytelwein), [3] relates the hold-force to the load-force if a flexible line is wound around a cylinder (a bollard, a winch or a capstan).
In fluid dynamics, the lift coefficient (C L) is a dimensionless quantity that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. A lifting body is a foil or a complete foil-bearing body such as a fixed-wing aircraft.
Lift is proportional to the density of the air and approximately proportional to the square of the flow speed. Lift also depends on the size of the wing, being generally proportional to the wing's area projected in the lift direction. In calculations it is convenient to quantify lift in terms of a lift coefficient based on these factors.
These inspections should be carried out at 6 monthly intervals for all lifting items and at least every 12 months for those that could be covered by PUWER, although a competent person may determine different time scales. Standards state that as a minimum; Every six months for lifting equipment used for lifting/lowering persons.
There are adequate load case coefficients available to estimate sling angle load amplification, suction from the casting bed, and various dynamic transportation load estimates. Load resistance factors of safety , FOS, set out in the Australian Code would typically denote a FOS of 5.0 for re-usable lifting equipment and an FOS of 2.5 for a ...
As stalling is due to wing loading and maximum lift coefficient at a given altitude and speed, this limits the turning radius due to maximum load factor. At Mach 0.85 and 0.7 lift coefficient, a wing loading of 50 lb/sq ft (240 kg/m 2) can reach a structural limit of 7.33g up to 15,000 feet (4,600 m) and then decreases to 2.3g at 40,000 feet ...
The Kutta–Joukowski theorem is a fundamental theorem in aerodynamics used for the calculation of lift of an airfoil (and any two-dimensional body including circular cylinders) translating in a uniform fluid at a constant speed so large that the flow seen in the body-fixed frame is steady and unseparated.