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- DictionaryLoad fac·tor/lōd ˈfaktər/
noun
- 1. the ratio of the average or actual amount of some quantity and the maximum possible or permissible.
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What is load factor?
What is the load factor of an aircraft?
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Load factor is defined as the ratio of the average load over a given period of time to the maximum demand (peak load) occurring in that period.
Dec 3, 2017 · The load factor of an aircraft describes the mass loading of an aircraft as a multiple of its weight. The same definition applies if we are speaking about an aircraft component: the load factor, here called the local load factor, will be the mass loading of that component as a multiple of that component's weight.
- The load factor is the total acceleration you feel, pointing downwards. In straight and level flight, the load factor is 1: you only feel the accel...
- If you are flying straight and level, the weight of your plane is in equilibrium with the lift, and the load factor is lift/weight = 1. Imagine th...
- Load factor is simply Aerodynamic Lift divided by aircraft weight, or more correctly, by aircraft inertial mass as normalized by 1 "G" - (32.2 ft/s...
- As another answer stated, Load Factor is simply Aerodynamic Lift divided by aircraft weight. Note that if Aerodynamic Lift is known and weight is k...
- Okay. A lot of good answers up there. After going through all of them there was one question that still lingered in my mind. Why do we neglect th...
Load factor is an expression of how much energy was used in a time period, versus how much energy would have been used, if the power had been left on during a period of peak demand. It is a useful indicator for describing the consumption characteristics of electricity over a period of time.
Definition-Load factor(LF) is defined as the ratio of the average load to the maximum demand over a given period. The average power can be calculated by calculating the total energy consumed for that period and then dividing the total energy by the time period.
The ultimate load is the load factor applied to the aircraft beyond the limit load and at which point the aircraft material experiences structural failure (breakage). Load factors lower than the limit load can be sustained without compromising the integrity of the aircraft structure.
Mar 29, 2024 · Firstly, load factor is a ratio, so there are no units to consider, even though it is often expressed as g. Secondly, it's simply the ratio of the lift provided by the lifting surfaces divided by the total weight of the aircraft. In straight and level flight, the load factor is 1.
A load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft (e.g., lift/weight). For example, a load factor of 3 means the total load on an aircraft’s structure is three times its gross weight.
