Part 1A cantilever beam supports the loads shown. The cross-sectional dimensions of the shape are also shown. Assume a = 0.4m. PA=2.0 kN, Pe= 6.0 kN, Pe- 2.5 kN, d = 115 mm, by= 85 mm, t,= 6 mm, tw= 10 mm. Determine(a) the maximum vertical shear stress.(b) the maximum compression bending stress.(c) the maximum tension bending stress.See the coordinate system for the beam in the problem figure with the origin of the x axis at the fixed support. Consider fourpoints along the beam's axis:Point A at x- 1.2 mPoint Bat x = 0.8 mPoint Cat x = 0.4 mPoint Dat x-0Break the beam into three segments: AB, BC, and CD. Enter the shear force in each segment with its correct sign based on thecoordinate system in the problem figure and the sign convention for shear forces in Chapter 7.Answers: Enter the maximum shear force magnitude in the beam. Since this is a magnitude, enter a positive value.Answer: VmaxeTextbook and MediaSave for LaterAttempts: 0 of 5 used Submit AnswerPart 3Enter the bending moment at four critical x-locations:Mpis the moment at x-0Mc is the moment at x = 0.4 mMg is the moment at x- 0.8 mMa is the moment at x- 1.2 mEnter each bending moment with its correct sign based on the coordinate system in the problem figure and the sign conventionfor bending moments presented in Chapter 7.Answers:MAkN-mkN-mMckN-mMp-kN-mPart 5Break the cross-sectional area into two areas:(1) Top horizontal flange with rectangular cross-section 85 mm x 6 mm.(2) Vertical stem with rectangular cross-section 10 mm x 109 mm.Find the areas and the centroid locations in the y-direction for each area. Enter the centroid locations, y; and y2, as measured withrespect to a reference axis at the bottom of the cross-section. In other words, let y-0 at the bottom edge of the vertical stem.Answers:mm?,mmmm?. v2"mmeTextbook and Media

Answered: Image /qna-images/answer/e1951d81-9f22-4cc1-b61b-162bf7e4fe44.jpg

Part 1 A cantilever beam supports the loads shown. The cross-sectional dimensions of the shape are also shown. Assume a = 0.4 m, PA= 2.0 kN, Pe= 6.0 kN, Pe- 2.5 kN, d = 115 mm, by= 85 mm, t;= 6 mm, tw= 10 mm. Determine (a) the maximum vertical shear stress. (b) the maximum compression bending stress. (c) the maximum tension bending stress. Pc See the coordinate system for the beam in the problem figure with the origin of the x axis at the fixed support. Consider four points along the beam's axis: Point A at x- 1.2m Point Bat x = 0.8 m Point Cat x= 0.4 m Point Dat x-0 Break the beam into three segments: AB, BC, and CD. Enter the shear force in each segment with its correct sign based on the coordinate system in the problem figure and the sign convention for shear forces in Chapter 7. Answers:

Part 1 A cantilever beam supports the loads shown. The cross-sectional dimensions of the shape are also shown. Assume a = 0.4 m, PA= 2.0 kN, Pe= 6.0 kN, Pe- 2.5 kN, d = 115 mm, by= 85 mm, t;= 6 mm, tw= 10 mm. Determine (a) the maximum vertical shear stress. (b) the maximum compression bending stress. (c) the maximum tension bending stress. Pc See the coordinate system for the beam in the problem figure with the origin of the x axis at the fixed support. Consider four points along the beam's axis: Point A at x- 1.2m Point Bat x = 0.8 m Point Cat x= 0.4 m Point Dat x-0 Break the beam into three segments: AB, BC, and CD. Enter the shear force in each segment with its correct sign based on the coordinate system in the problem figure and the sign convention for shear forces in Chapter 7. Answers:

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

4. A force Q is applied to a rectangular member with a size of 3oomm x 450mm. Q is located 37-5mm left and 6omm north of the center of gravity and induces a stress of 1.75 MPa compression at point A. a) What is the axial load at Q in kN b) What is the stress induced at point C & D in MPa A B
6
PROBLEM No. 2 The rigid bar ABCD of negligible weight is initially horizontal, and the steel rods attached at A and C are stress-free. If a 20-kip load is applied, determine the vertical displacement in the bar at A and C that will cause a stress in the rod at C to be 50 ksi. Indicate the direction of movement. Use E = 29x106 psi for steel. (Provide FBD and movement diagram in your computation). A = 0.5 in.? 3 ft | A B D | 20 kips te 2 ft -→-- 2 ft -→l 4 ft 4 ft A = 0.75 in.²
The rigid beam ABC is supported by a pin connection at C and by steel rod (1), which has a diameter of 7 mm. If the normal stress in rod (1) must not exceed 215 MPa, what is the maximum uniformly distributed load w that may be applied to beam ABC? What is the allowable force in road (1)? Use dimensions of a = 350 mm, b = 700 mm, and c = 525.0 mm.
A 62.6-kN vertical load P is applied at the corner of the square cross section of the steel compression member AB, which is free at its top A and fixed at its base B. Knowing that for the grade of steel used oy=345 MPa and E= 200 GPa, and using the allowable-stress method, determine the smallest allowable dimension d. B D 1.5 m The smallest allowable dimension dis mm.
Please answer B only.
Problem 1: Obtain a preliminary design of the shaft by performing the following tasks. Note that forces T=2880 N and T;=432 N. The maximum bending moment is atx= 230 mm (point B), and it equals M= 698.3 N•m completely reversed, where the torque is constant at 612 N.m at the same point. The shaft material is AISI 1020 CD steel. Take the stress concentration conditions at B to be Shoulder fillet-sharp, with notch radius r=0.6 mm (Table 7-1). y 230 mm T, 280 mm 30-mm dia. T C 300 mm 250-mm dia. 400-mm dia. 270 N 1800 N a) Sketch a general shaft layout in 2D (x – y axes), including all components and torques, then calculate all reactions. b) Based on the current shaft dimensions and using only forces at B and C, find the lowest critical speed of the shaft. c) Discard the indicated shaft diameter and use DE-Goodman criteria to determine the critical diameter of the shaft based on infinite fatigue life with a design factor n of 1.5. (Take the same value of endurance limit as that used in…
Need help ASAP Determine the max flexural stress in MPa
A simply supported wood beam that is 14.1 m long carries a 47 kN concentrated load at B. The cross-sectional dimensions of the beam are b = 160 mm, d = 360 mm, a = 70 mm, andc = 20 mm. Section a-a is located at x = 2.4 m from B. (a) At section a-a, determine the magnitude of the shear stress in the beam at point H. (b) At section a-a, determine the magnitude of the shear stress in the beam at point K. (c) Determine the maximum horizontal shear stress that occurs in the beam at any location within the entire span. (d) Determine the maximum tensile bending stress that occurs in the beam at any location within the entire length. y H a a A В K L 2L Answer: (a) TH = i kPa (b) TK = i КРа (c) Tmax = i kPa (d) Omax MPa i 13
The beam shown below has a cross section of channel shape with width b=200 mm and height h=80 mm, the web thickness is t=12 mm. Determine the maximum tensile and compressive stresses in the beam due to uniform load. And draw. 200 mm 3.2KN/ 2 KN.M BO 80mm 12mm 3m 1.5m
make it understanda
Consider a cantilevered beam which is made of two identical. rectangular sections, a force P is applied at free end. 11) if A and B are not clued together, determine the bending stress distribution at a-a cross section, draw o Chint: each section carries P/ and label the Tout at the outest fibers. * 0.5m a 12) if we weld the two A & B together along the member length. determine the bending stress distribution, draw and laber. m ✓ P=1kw A 181- дет B зст