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  2. Load factor (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Load_factor_(aeronautics)

    The load factor, and in particular its sign, depends not only on the forces acting on the aircraft, but also on the orientation of its vertical axis. During straight and level flight, the load factor is +1 if the aircraft is flown "the right way up", [2]: 90 whereas it becomes −1 if the aircraft is flown "upside-down" (inverted). In both ...

  3. Passenger load factor - Wikipedia

    en.wikipedia.org/wiki/Passenger_load_factor

    Specifically, the load factor is the dimensionless ratio of passenger-kilometres travelled to seat-kilometres available. For example, say that on a particular day an airline makes 5 scheduled flights, each of which travels 200 kilometers and has 100 seats, and sells 60 tickets for each flight. To calculate its load factor:

  4. Stall (fluid dynamics) - Wikipedia

    en.wikipedia.org/wiki/Stall_(fluid_dynamics)

    The normal stall speed, specified by the V S values above, always refers to straight and level flight, where the load factor is equal to 1g. However, if the aircraft is turning or pulling up from a dive, additional lift is required to provide the vertical or lateral acceleration, and so the stall speed is higher.

  5. Flight envelope - Wikipedia

    en.wikipedia.org/wiki/Flight_envelope

    A chart of velocity versus load factor (or V-n diagram) is another way of showing limits of aircraft performance. It shows how much load factor can be safely achieved at different airspeeds. [3] At higher temperatures, air is less dense and planes must fly faster to generate the same amount of lift.

  6. Limit load (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Limit_load_(aeronautics)

    For aircraft specification calculation in aeronautics, limit load (LL) is the maximum design load expected as the maximum load any aircraft will see during its lifetime, [1]

  7. Flight control modes - Wikipedia

    en.wikipedia.org/wiki/Flight_control_modes

    The flight mode of normal law provides five types of protection: pitch attitude, load factor limitations, high speed, high-AOA and bank angle. Flight mode is operational from take-off, until shortly before the aircraft lands, around 100 feet above ground level. It can be lost prematurely as a result of pilot commands or system failures.

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  9. Load factor - Wikipedia

    en.wikipedia.org/wiki/Load_factor

    Load factor (aeronautics), the ratio of the lift of an aircraft to its weight; Load factor (computer science), the ratio of the number of records to the number of addresses within a data structure; Load factor (electrical), the average power divided by the peak power over a period of time; Capacity factor, the ratio of actual energy output to ...