## Deflection of a Fixed Beam With Uniformly Distributed Load

Deflection of a Fixed Beam With Uniformly Distributed Load The maximum deflection of beams occurs where slope is zero. Slope of the beam is defined as the angle between the…

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# aerospace

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Deflection of a Fixed Beam With Uniformly Distributed Load

Deflection of a Fixed Beam With Uniformly Distributed Load The maximum deflection of beams occurs where slope is zero. Slope of the beam is defined as the angle between the…

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Circulation at Origin in finite Wing

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Induced Angle of Attack

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Horizontal tail volume coefficient

The downwash produced by the circulation of the bound vortex of the wing is zero at the wing and therefore does not contribute to the induced drag.

The downward vertical angle between the horizontal and the velocity (relative to the wing of an aircraft) of the airstream passing over the wing

For a horizontal tail or canard, the pitching moments which must be countered are most directly related to the wing mean chord (Cw). This leads to the "horizontal tail volume coefficient,