1) F=36 kN single load, M=48 kN.m moment and w=20 kN/m distributed load act on the beam whose loading condition is given in the The length Lis also given as L=3 m. The cross-sectional properties of the beam are; body height y a =210 mm , body thickness xg =14 nge width x f= 173 mm, flange height y f=14 mm . Point P on the section is tocated just above the flange-body junction. It is o determine the stress state at point P in the section taken from the B line of the beam. According to this; w kN/m F kN M kN.m E B C 2L L L P Yg Xg a 1-A) B at a point of cutting force (V 8 ) to find. ( Write your result in kN.) 1-В), B at a point of bending moment (M 8 ) you find. ( Write your result in kN.m.) Find the moment of inertia of the beam section .( Do your operations by converting the lengths to meters. Take at least 4 1-C) the decimal part of your result and use the expression E for the decimat part. Write it as 5E-3 instead of 0.005 .)
1) F=36 kN single load, M=48 kN.m moment and w=20 kN/m distributed load act on the beam whose loading condition is given in the The length Lis also given as L=3 m. The cross-sectional properties of the beam are; body height y a =210 mm , body thickness xg =14 nge width x f= 173 mm, flange height y f=14 mm . Point P on the section is tocated just above the flange-body junction. It is o determine the stress state at point P in the section taken from the B line of the beam. According to this; w kN/m F kN M kN.m E B C 2L L L P Yg Xg a 1-A) B at a point of cutting force (V 8 ) to find. ( Write your result in kN.) 1-В), B at a point of bending moment (M 8 ) you find. ( Write your result in kN.m.) Find the moment of inertia of the beam section .( Do your operations by converting the lengths to meters. Take at least 4 1-C) the decimal part of your result and use the expression E for the decimat part. Write it as 5E-3 instead of 0.005 .)
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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