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A trimmed flight condition is perhaps best thought of as an equilibrium condition. The simplest trim condition is straight-and-level flight, in which the forces (weight, propulsive, aerodynamic) balance and the moments (aerodynamic and propulsive) sum to zero3.
In this particular trim, the accelerations and angular accelerations are all zero. An aircraft could also be trimmed in a steady banked level turn, a climb, a powered descent, though note that (for example) in a steady turn, the forces and moments will not be balanced because a resultant force and a resultant moment are required to provide the necessary centripetal acceleration (rate-of-change of momentum) and the necessary precession of the angular momentum vector (rate-of-change of angular momentum).
Effects of Temperature and Altitude. Cold and/or Low On cold days the air density will increase. If the engine has a ‘part throttle rating' and the throttle is advanced to
Shell-mould Casting is variant of the resin bonded sand technique for casting steel, iron or non-ferrous alloys. The mould is made by a mixture of fine sand (100 - 150 mesh) an
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Maintenance of Aircraft under “B” conditions: The maintenance of aircraft flying under "B" conditions must be adequate in relation to the number and duration of the flight
dual input balanced ouput differential output
name the functions of the CIPM
Fins vs Canards Canard control - Good lift/latax control for moderate angles of attack. - Shed vortices can interfere with tail to generate roll moment. - Tendency to stall
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