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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 ...
Cockpit controls and instrument panel of a Cessna 182D Skylane. Generally, the primary cockpit flight controls are arranged as follows: [2] A control yoke (also known as a control column), centre stick or side-stick (the latter two also colloquially known as a control or joystick), governs the aircraft's roll and pitch by moving the ailerons (or activating wing warping on some very early ...
Flight dynamics; Energy states; Load factor (flight mechanics) Aerodynamic flight envelope; Aerodynamic causes: Angle of attack and stall; Camber; Control surface fundamentals; Spoiler-type devices; Trim; Lateral and directional aerodynamic considerations; Angle of sideslip; Wing dihedral effects; Pilot-commanded sideslip; Crossover speed ...
Passenger load factor is an important parameter for the assessment of the performance of any transport system. Almost all transport systems have high fixed costs, and these costs can only be recovered through selling tickets. [2] Airlines often calculate a load factor at which the airline will break even; this is called the break-even load ...
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.
Load factor may refer to: 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
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Flight envelope diagram. 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.