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In the previous discussion, we investigated the static aeroelastic behaviour of straight (unswept) wings. These wings are characterised by an effective decoupling of wing bending and wing twist ruling out the influence of bending as a factor. Two critical dynamic pressures (or equivalently flight speeds) have been presented representing the torsional divergence and control surface reversal phenomena. A third important critical dynamic pressure is related to the dynamic aeroelastic instability of flutter, which will be discussed later on. For straight wings, the flutter dynamic pressure is most critical, while information of torsional divergence and control surface reversal phenomena are important to establish the overall aeroelastic picture of the aircraft.For swept wings, bending has an important and complicating impact on the aeroelastic stability characteristics. These will be presented qualitatively in the following.
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Wire Drawing involves pulling the metal through a die by means of tensile force applied to the exit side of the die. A typical wire drawing operation is shown in fig.
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DIVERGENT DUCT A divergent duct widens out as the airflow progresses through it. At subsonic speeds the effect of this kind of duct is to decrease the velocity and increase the p
Fuel properties of Aircraft: EASE OF FLOW The ease of flow of a fuel is mainly a question of viscosity, but impurities such as ice, dust, wax, etc., may cause blockages in
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Vibrating beam accelerometer The electrodes are driven by a high frequency voltage (1 MHz). The displacement is measured using a phase detector from the change of capacitance b
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