The floor of an apartment building shown is subjected to a uniformly distributed dead load of 1.5 kPa and a uniformly distributed live load of 1.9 kPa over its surface area. Determine the factored (LRFD) reaction (kN) of girder AF that will be transferred to the column at A. Girder Floor beam Column A Į B FH G L H M -4 at 7.5 m = 30 m D N E 2 at 12 m = 24 m

The floor of an apartment building shown is subjected to a uniformly distributed dead load of 1.5 kPa and a uniformly distributed live load of 1.9 kPa over its surface area. Determine the factored (LRFD) reaction (kN) of girder AF that will be transferred to the column at A. Girder Floor beam Column A Į B FH G L H M -4 at 7.5 m = 30 m D N E 2 at 12 m = 24 m

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

1 - Determine the maximum shearing stress in the beam for the loading shown in the figure. The same beam cross-section was used in HW 5. 2 KN 0.5m- 1KN - 0.5m 107 30 30 T dimensions in mm lok beam cross-section
A simple pin-connected truss is loaded and supported as shown in the figure shown. All members of the truss are aluminum pipes that have an outside diameter of 60 mm and a wall thickness of 4 mm. Determine the normal stress in truss AC in MPa. 1.5 m O 62.5 63.9 O 71.2 66.4 1.0 m B 3.3 m 15 kN 12 kN
1.0 Earthquake Load Combinations: Strength Design This example demonstrates the application of the strength design load combinations that involve the seismic load E given in NSCP 2015 ion 208.5.1.1. This will be done for the moment resisting frame shown below: Find the following: Zone 4 C₂ = 0.44 /= 1.0 p=1.1 f₁=0.5 Beam Moment at A Column C-D axial load Column Moment at C Dead Load D Beam A-B and Column C-D are elements of the special moment-resisting frame. Structural analysis has provided the following individual beam moments at A, and the column axial loads and moments at C due to dead load, office building live load, and lateral seismic forces. 135 kN-m 400 KN 55 kN-m C Live Load L 1. 2. 65 kN-m 180 KN 30 kN-m Strength design moment at beam end A. Strength design axial load and moment at column top C. Lateral Seismic Load En 165 kN-m 490 KN 220 kN-m
A rigid plate C is used to transfer a 20-kip load P to a steel (E = 30,000 ksi) rod A and to an aluminum alloy (E = 10,000 ksi) pipe B as shown. The supports at the top of the rod and the bottom of the pipe are rigid, and the materials were unstressed before the load was applied. The cross-sectional areas of rods A and pipe B are 0.80 in2 and 3.00 in2 respectively. Determine The normal stress in rod A in ksi, The normal stress in pipe B in ksi and The displacement of plate C in inches. Note: Draw the Free Body Diagram, include the units/dimensions, use the proper formula and round-off all the answers and final answers to 5 decimal places.
As shown in the figure below, determine the internal loadings at point C. В 0.1 m 0.5 m C -0.75 m - -0.75 m -0.75 m (FN x 100) N EN = 78
1 - Determine the maximum shearing stress in the beam for the loading shown in the figure. The same beam cross-section was used in HW 5. 2 KN 0.5m 1 KN * 0.5m 30 30 T dimensions in mm 10k beam cross-section
For the truss shown in figure, (a) determine the stress developed in member FH if it has a cross-sectional area of 1200 ??? (b) determine the stress developed in member AB if it has a cross-sectional area of 1100 ???.
Find the required value of plastic moment capacity in the continuous beam shown in fig. The loads shown in fig are the collapse loads
The member shown has a rectangular cross section, determine the state of stress that loading produces at point C. 1.5m 1c T 250mm 2.5m 125mm 1.5m 50mm 4m + 2m 50kN/m
The cantilever T- beam is loaded as shown in the figure. Ti 80 mm 40 kN/m NA --- 120 mm 2.0 m INA = 30x105 mm What is the value of fleure stress in a distance 1.20 m from the free end at the topmost fiber of the beam section?
A prismatic bar is fastened between two rigid walls at A and B and subjected to loads as shown in figure below. Determine the reactions at supports. D R₁4 ← 100 mm C 13.6 KN 200 mm 27.2 kN 300 mm Ra
Two solid cylindrical road AB and BC are welded together at B and loaded as shown. Knowing that d₁ = 30mm (for AB) and d₂ = 50mm (for BC), find the average normal stress in each road and the total deformation of road AB and BC. E=220GPa 60KN A 125kN- 125kN- -0.9m B