The thrust equation relates the thrust produced by a propulsion system to the mass flow rate of the exhaust gases and their velocity. In SI (International System of Units) units, the thrust equation is typically expressed as    F is the thrust in Newtons (N). m (pronounced “m-dot”) is the mass flow rate of […]
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The drag equation calculates the force of drag experienced by an object moving through a fluid, such as air or water. The drag force depends on various factors, including the object’s shape, size, speed, and the properties of the fluid. The general form of the drag equation is:       Fd​
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The lift equation is fundamental in aerodynamics and is used to calculate the lift force required to keep an object, like an aircraft, in the air based on its design, the surrounding air density, the reference area, and its velocity relative to the air. Lift Force (L) is measured in Newtons (N). Coefficient of Lift
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