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Engineering Mechanics: Reactions at A & C (α=0, α=30°) - Solved Problem

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(a) RA=60lb↑ RC=160lb←,60lb↓
(b) RA=97.4lb(Normal to plane)
RC=208.7lb←, 84.4lb↓
RA=276.8N(45º), RC=378.0N(59º)
128N
77N

0

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