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By David J. Peery

Nonetheless correct a long time after its preliminary e-book, this mythical reference textual content on plane tension research is taken into account the easiest ebook at the topic. It emphasizes uncomplicated structural thought, which is still unchanged with the advance of recent fabrics and development tools, and the applying of ordinary ideas of mechanics to research of plane constructions.

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Extra resources for Aircraft Structures

Sample text

From this cr0108 section? 2. Inertia Forces on Rota- Bodies. In the preceding discussion all parts of the rigid body were moving in straight, parallel lines and had equal velocities and accelerations. In many engineering problems it is necessary to consider the inertia forces acting on a rigid body which has other types of motion. In many cases where the elements of a rigid body are moving in curved paths they are moving in such a way that each element movea in only one plane, and all elements move in parallel planes.

What is the shear and bending moment on a vertical section AA, if the weight forward of this section is 2,000 lb and has a center of gravity 40 in. from this cr0108 section? 2. Inertia Forces on Rota- Bodies. In the preceding discussion all parts of the rigid body were moving in straight, parallel lines and had equal velocities and accelerations. In many engineering problems it is necessary to consider the inertia forces acting on a rigid body which has other types of motion. In many cases where the elements of a rigid body are moving in curved paths they are moving in such a way that each element movea in only one plane, and all elements move in parallel planes.

All elements of the airplane move in planes parallel to the plane of symmetry. Any type of plane motion can be considered as a rotation about some instantaneous axis perpendicular to the planes of motion, and the following equations for inertia forces are derived on the assumption that the rigid body is rotating about an instantaneous axis perpendicular to a plane of symmetry of the body. The inertia forces obtained may be used for the pitching motion of an airplane, but when used for rolling or yawing motions it is necessary first to obtain the principal axes and moments of inertia of the airplane.

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