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The rocket experiences a wind gust during ascent, causing unwanted loading. To prevent rotation, the resultant moment about the center of mass must vanish. This can be achieved by varying the orientation of the thrust vector with respect to the vertical axis. The document asks (a) what relationship must exist between thrust, wind force, and their distances from the center of mass to satisfy this requirement, and (b) to determine the internal shear force and bending moment at quarter and three-quarter points

Author

최수아

Language

EN