The cantilevered handle in the figure is made from mild steel that has been welded at the joints. For Fx= -150 lbf, Fy= 0, and F₂=-50, use superposition to determine the deflection along the x-axis at D. The part dimensions are as follows: dAB= 1.12 in, dCD= 0.625 in, t = 0.125 in and h = 0.75 in.

The cantilevered handle in the figure is made from mild steel that has been welded at the joints. For Fx= -150 lbf, Fy= 0, and F₂=-50, use superposition to determine the deflection along the x-axis at D. The part dimensions are as follows: dAB= 1.12 in, dCD= 0.625 in, t = 0.125 in and h = 0.75 in.

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

weight = 3758.0678Kg Leght is given the the FBD Inirta is = 39.2(10^6)mm^6 Gpa = 200 Please calculate the maximum deflection on the beam with you own sellected fomular that matches the digram
Q2: The simply supported beam shown as Figure 5. below is subjected to Loading as shown on the Figure. Using singularity function method. Find the maximum Lenght (L) so that the max. deflection is not greater than 30mm for the Beam.. The flexural rigidity (El) of Beam section El = 50*103 KN.m?2 “4m L Sm
The equation for the deflected shape of a beam carrying a UDL and simply supported at the ends is given below: 1 y = -2x + EI + 36.x Determine the load carrying capacity of the beam and draw the BMD and SFD. The unit of El is kNm2.
Compute the deformation of the beam using area method:E= 200 GPa I= 1000 x 106 mm4
A ruler is clamped at 0.36 ку = weight weight is at deflection at deflection at It is What are ruler as x=17cm uniform bean a x = 3cm and x = 30cm x=16cm is x = 20cm is 1.5mm Inn the value functions for modelling the beam? (length, load, boundary Conditions • Estimate the flexural rigidity of the ruler.
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I = 1640 in.*). For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 240 kip-ft, P = 11 kips, LAB = 3.4 ft, Lgc = 5.1 ft. P MA A B C LAB LBC Answer: (a) VA = in. (b) Vg = in.
Topic: BEAM BEARING PLATES AND COLUMN BASE PLATES Please solve your Solution in a handwritten Note: It should be handwritten pleaseeee A w24 X55 is used as a beam with a length of 6m. The beam is supported by a bearing plate of 300 mm x 200 mm x 30 mm on the wall having a thickness of 250 mm.Properties: d=598.68mmbf = 177.93 mmtw =10.03mm k=33.34 mmtf = 12.83mmFy = 250 MPaQuestions:1. Determine the design strength for web local yielding.2. Determine the design strength for web crippling.
A beam of the cross section shown is extruded from an aluminum alloy for which Oy= 250 MPa and ou= 450 MPa. Using a factor of safety of 3.00, determine the largest couple that can be applied to the beam when it is bent about the z-axis. Take x = 18 mm. M₂ 24 mm 80 mm 24 mm X The largest couple that can be applied to the beam when it is bent about the z-axis is kN-m.
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I = 1860 in.“]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 180 kip-ft, P = 12 kips, LAB = 3.8 ft, LBC = 5.7 ft. MA A B LAB LBC Answer: (a) VA = in. (b) VB = in.
The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; | = 1960 in.4]. For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA = 160 kip-ft, P = 17 kips, LAB = 6.4 ft, LBC = 9.6 ft. AP MA A B C LAB LBC Answer: (a) VA = in. (b) VB = in.
А L B 425 mm C 1,000 mm V P A steel bar (1) and an Aluminum bar (2) are connected to a rigid angle ACD. Assuming: • Steel [E = 200 GPa] bar (1) is 6mm x 40mm x 600mm long. • Aluminum [E = 70 GPa] bar (2) is 10mm x 40mm x 600mm long. Poisson's ratio, v = 0.35 • A distance L of 500mm. a)Determine the force P (in kN) required to stretch the Aluminum bar by 1mm. Enter the force, P, into the d21 answer box (in kN, 3 sig digs). b) Determine the final width and thickness of the Aluminum bar. (1) Your Answer:
O FS = 2.4 O FS = 2.2 Consider a simple supported beam subjected to the load shown. The beam has a solid square cross-section with edge "a", and made of steel alloy having a yielding tensile and compressive strength of oy = 400 MPa. Determine its minimum required edge "a" for a factor of safety against yielding FS = 2.5. The area moment of inertia of that section about its neutral axis N.A. is INA = b.h³/12. of 3 kN 2 kN/m D 6 m + Select one: 5:37 PM 86°F Light rain ENG 6/18/2021 hp