/. u/es ug up w21EA W21 x 50 spans 11.0 m on a simple span. The compression flange is laterally supported at the third points. A36Steel is used.A = 9,484 mm²b₁ = 165.9 mmProperties of W21 x 50 sectiontw = 9.7 mmIx=409.57 x 10 mmIy = 10.36 x 10 mmSx = 1548.58 x 10³ mm³Sy = 125.20 x 10³ mm³d=529.1 mmtf = 13.6 mmw = 0.73 kN/ma) Determine the allowable bending stress of this beam.b) Determine the allowable superimposed uniformly distributed load be place on this beam.

Given the section of beam W 21* 50 and its properties. Fy for A36 taken as 248 MPa.

A W21 x 50 spans 11.0 m on a simple span. The compression flange is laterally supported at the third points. A36 Steel is used. Properties of W21 x 50 section tw = 9.7 mm A = 9,484 mm² b₁ = 165.9 mm S₂ = 1548.58 x 10³ mm³ Sy = 125.20 x 10³ mm³ I₂ = 409.57 x 10 mm d=529.1 mm Iy = 10.36 x 10 mm t₁ = 13.6 mm w = 0.73 kN/m a) Determine the allowable bending stress of this beam. b) Determine the allowable superimposed uniformly distributed load be place on this beam.

A W21 x 50 spans 11.0 m on a simple span. The compression flange is laterally supported at the third points. A36 Steel is used. Properties of W21 x 50 section tw = 9.7 mm A = 9,484 mm² b₁ = 165.9 mm S₂ = 1548.58 x 10³ mm³ Sy = 125.20 x 10³ mm³ I₂ = 409.57 x 10 mm d=529.1 mm Iy = 10.36 x 10 mm t₁ = 13.6 mm w = 0.73 kN/m a) Determine the allowable bending stress of this beam. b) Determine the allowable superimposed uniformly distributed load be place on this beam.

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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