FIGURE P1.38/39 P1.39 WP Two aluminum plates, each having a width b = 5.0 in. and a thickness t = 0.75 in., are welded together as shown in Figure P1.38/39. Assume that a = 2.0 in. Specifications require that the normal and shear stress magnitudes acting in the weld material may not exceed as bei and 24 bei respectively Determine the largest avial load R that can be applied to the aluminum plates
FIGURE P1.38/39 P1.39 WP Two aluminum plates, each having a width b = 5.0 in. and a thickness t = 0.75 in., are welded together as shown in Figure P1.38/39. Assume that a = 2.0 in. Specifications require that the normal and shear stress magnitudes acting in the weld material may not exceed as bei and 24 bei respectively Determine the largest avial load R that can be applied to the aluminum plates
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FIGURE P1.38/39.
P1.39 (WP Two aluminum plates, each having a width b = 5.0 in. and a thickness t = 0.75 in., are welded together as shown in Figure P1.38/39. Assume that a = 2.0 in. Specifications require that the
normal and shear stress magnitudes acting in the weld material may not exceed 35 ksi and 24 ksi, respectively. Determine the largest axial load P that can be applied to the aluminum plates.
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