A cantilever beam carries the force and couple shown in Fig. P-552. Determine the ff. -Total Area of Beam Section -Neutral axis from the Bottom of beam Section -Moment of Inertia at Neutral axis -Compressive Bending Stress -Tensile Bending Stress 5 kip/ft 30 kip-ft LA L TAT 11 ft 11 ft Figure P-552 Please help. Flange b = 11 inches Web b = 2 inches. 11 in 2 in

A cantilever beam carries the force and couple shown in Fig. P-552. Determine the ff. -Total Area of Beam Section -Neutral axis from the Bottom of beam Section -Moment of Inertia at Neutral axis -Compressive Bending Stress -Tensile Bending Stress 5 kip/ft 30 kip-ft LA L TAT 11 ft 11 ft Figure P-552 Please help. Flange b = 11 inches Web b = 2 inches. 11 in 2 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

1. The location of the centroid measured from the top fiber in (mm) 2. The moment of inertia about the centroidal x axis (mm) 3. The maximum compressive stress in (MPa) 4. The maximum tensile stress in (MPa) 5. The maximum shear stress at junction between the web and the flange (within the web) (MPa) 6. The maximum shear stress at the neutral axis in (MPa)
Determine the following : 1. Vertical reaction of hinge at A in pounds, Av 2. Horizontal reaction of hinge at A(lbs), Ah 3.Maximum shear value(lbs) 4. Maximum moment value (lb-ft)
A beam has a concentrated load (Pu) at midspan and has a fixed support at both ends. If the beam properties are given below, what is the stress at bottom of the beam section at 3.41 from the support. (MPa) Properties: Beam width = 206 mmBeam height = 495 mmPu = 66.2 kNSpan of the beam = 11 mPrestressing force = 335 kNeccentricity = 105 mm
Refer to the photo provided and please make sure your handwriting is readable a = 1.01 m b = 2.02 m c. 1.505 m d. 4.505 m P1 = 6.06 kN P2 = 24.04 kN 1. Compute the resultant reaction at I in kN. 2. Compute force member DE in kN 3. Compute normal stress in member CE in kN/m2 if the value of the area is A mm2.
Q6. For the beam and loading shown in Fig.(2). Consider section (n-n) and determine A. The largest shearing stress in that section. B. The shearing stress at point (a) (1 in.) below the top face. C. The shearing stress at point in the top face Load = 65 kips
an 8 m long steel is pinned at the top and fixed at the bottom. the column is provided with lateral support 3m from the top in the weak direction. the properties of the column section are as follows: ix = 178.1x10^6 mm^4 ly = 18.8x10^6 mm^4 a = 8129 mm^2 fy = 400 mpa a. what is the critical effective slenderness ratio? %3d %3d b. what is the buckling stress of the column? c. calculate the critical load pc in kn
1. If the shear at a point 1m from the roller support is equal to -217.65765765766kN, determine the value of "w". 2. Determine the deflection at point 3.2m from the hinge support. 3. Determine the deflection at point 1m from the roller support.
The wire BC has a diameter of 0.175 in. and the material has the stress-strain characteristics shown in the figure. Determine the vertical displacement of the handle at D if the pull at the grip is slowly increased and reaches a magnitude of (a) P= 480lb, (b) P= 700lb. Assume the bar is rigid.
A cantilever beam of IPN 300 section and length L=3m supports a slightly inclined load P=2,5KN at the free end (see Figure Q2).2.1 Plot a graph of the stress ?? at point A as a function of the angle of inclination ?. [16]2.2 Plot a graph of the angle ?, which locates the neutral axis n-n, as a function of the angle ?. See Table F-2 of Appendix F for the dimensions and properties of the beam (When plotting the graphs, let ? vary from 0 ?? 10°).
9. A steel strut S serving as a brace for a boat hoist transmits a compressive force P = 62 kN to the deck of a pier as shown in the figure. The strut has a hollow square cross section with wall thickness t = 8 mm and the angle θ between the strut and the horizontal is 43°. A pin through the strut transmits the compressive force from the strut to two gussets G that are welded to the base plate B. Four anchor bolts fasten the base plate to the deck. The diameter of the pin is dpin = 15 mm, the thickness of the gussets is tG = 12 mm, the thickness of the base plate is tB = 10 mm, and the diameter of the anchor bolts is dbolt = 10 mm. Determine the bearing stress between the anchor bolts and the base plate in MPa. Round off to two decimal places.
The T-beam is subjected to a bending moment of M = 150 kip in. directed as shown. Determine the maximum bending stress in the beam and the orientation of the neutral axis. Make sure you check all possible points (corners) for max stress and/or state other reasoning for the point that you pick. Answer: [σmax = 3.33 ksi, β = -63.1°]
A beam has a uniform dead load and live load has a fixed support at both ends. If the beam properties are given below, what is the stress at bottom of the beam section at the midspan. (MPa) Properties: Beam width = 270 mmBeam height = 375 mmWLL = 14.38 kN/mWDL = 18.41 kN/mSpan of the beam = 8 mPrestressing force = 481 kNeccentricity = 103 mm