9.11 For the truss of Problem 8.51, determine the maximum tensile and compressive axial forces in member DI due to a concentrated live load of 40 k, a uniformly distributed live load of 4 k/ft, and a uniformly distributed dead load of 2 k/ft. A H B FIG.P8.51 X X -K C D 6 panels at 16 ft = 96 ft L E F G 14 ft 8 ft 12 ft
9.11 For the truss of Problem 8.51, determine the maximum tensile and compressive axial forces in member DI due to a concentrated live load of 40 k, a uniformly distributed live load of 4 k/ft, and a uniformly distributed dead load of 2 k/ft. A H B FIG.P8.51 X X -K C D 6 panels at 16 ft = 96 ft L E F G 14 ft 8 ft 12 ft
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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