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  2. Load factor (aeronautics) - Wikipedia

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

    When the load factor is +1, all occupants of the aircraft feel that their weight is normal. When the load factor is greater than +1 all occupants feel heavier than usual. For example, in a 2 g maneuver all occupants feel that their weight is twice normal. When the load factor is zero, or very small, all occupants feel weightless.

  3. Factor of safety - Wikipedia

    en.wikipedia.org/wiki/Factor_of_safety

    In engineering, a factor of safety (FoS) or safety factor (SF) expresses how much stronger a system is than it needs to be for an intended load.Safety factors are often calculated using detailed analysis because comprehensive testing is impractical on many projects, such as bridges and buildings, but the structure's ability to carry a load must be determined to a reasonable accuracy.

  4. Limit load (aeronautics) - Wikipedia

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

    The limit load can be found relatively easily by statistically analysing the data collected during the many hours of logged flights (which is continuously being gathered) but is generally predicted due to service of other aircraft before the design phase.

  5. 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.

  6. Ultimate load - Wikipedia

    en.wikipedia.org/wiki/Ultimate_load

    In engineering, the ultimate load [1] is a statistical figure used in calculations, and should (hopefully) never actually occur.. Strength requirements are specified in terms of limit loads (the maximum loads to be expected in service) and ultimate loads (limit loads multiplied by prescribed factors of safety).

  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.

  8. Man charged with murder after woman set ablaze on New York ...

    www.aol.com/news/depraved-behavior-leaders...

    On Wednesday, Hochul said that an additional 250 National Guard members will be deployed to New York City to bolster safety. She also announced that the MTA installed over 15,000 security cameras ...

  9. Flight envelope - Wikipedia

    en.wikipedia.org/wiki/Flight_envelope

    In aerodynamics, the flight envelope, service envelope, or performance envelope of an aircraft or spacecraft refers to the capabilities of a design in terms of airspeed and load factor or atmospheric density, often simplified to altitude. [1] [2] The term is somewhat loosely applied, and can also refer to other measurements such as maneuverability.