What do you mean by Endurance of Aircraft?
In aviation, endurance is the maximum length of time that an aircraft can spend in cruising flight. In other words, it is the amount of time an aircraft can stay in the air with one load of fuel. Endurance is different from range, which is a measure of distance flown. For example, a typical sailplane exhibits high endurance characteristics but poor range characteristics. Endurance can factor into aviation design in a number of ways. Some aircraft, require high endurance characteristics as part of their mission profile (often referred to as loiter time). Endurance plays a prime factor in finding out the fuel fraction for an aircraft. Endurance, like range, is also related to fuel efficiency; fuel-efficient aircraft will tend to exhibit good endurance characteristics.
How to Calculate Lift to drag ratio for maximum endurance in terms of max lift to drag ratio for prop-driven aircraft?
Lift to drag ratio for maximum endurance in terms of max lift to drag ratio for prop-driven aircraft calculator uses Lift to Drag ratio at maximum Endurance = 0.866*Maximum Lift to Drag ratio of Aircraft to calculate the Lift to Drag ratio at maximum Endurance, Lift to drag ratio for maximum endurance in terms of max lift to drag ratio for prop-driven aircraft is the lift to drag ratio of a plane at which the plane can achieve maximum endurance, but it also depends upon the maximum lift to drag ratio, it theoretically values 86.6% of maximum lift to drag ratio. Lift to Drag ratio at maximum Endurance is denoted by L/D_{(Emax)} symbol.
How to calculate Lift to drag ratio for maximum endurance in terms of max lift to drag ratio for prop-driven aircraft using this online calculator? To use this online calculator for Lift to drag ratio for maximum endurance in terms of max lift to drag ratio for prop-driven aircraft, enter Maximum Lift to Drag ratio of Aircraft (L/D_{max}) and hit the calculate button. Here is how the Lift to drag ratio for maximum endurance in terms of max lift to drag ratio for prop-driven aircraft calculation can be explained with given input values -> 25.98 = 0.866*30.