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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).
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Representing vectors in different axes All positions, velocities, momentums and accelerations are really relative positions, relative velocities, relative momentums and relativ
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3. Earthway Corporation has target capital structure of 60 percent common stock, 5 percent preferred stock and 35 percent debt. Its cost of equity is 12.5 percent, the cost of pr
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Economic Definition : Manufacturing increase the value of product. Technological Definition : Manufacturing is a process which gives required strength, shape and size of t
This Compression After Impact (CAI) test fixture was developed by the Boeing Company. The specimen, typically, but not necessarily, a quasi-isotropic laminate, is 6" long, 4" wide,
Interior noise is basically airborne or structure-borne. The excitation sources of vibratation and noise from engines can be divided as mechanical, combustion, and flow sources.
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Choked Nozzle Considering the formula for thrust under "choked" nozzle conditions: Thrust =(P-P 0 )A + WV j /g Where: P = Pressure P = Ambien
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