Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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Chapter 9, Problem 10P
To determine
Find the maximum tensile axial force in member BE and the maximum compressive axial force in member BF.
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1.3 Determine the largest weight W that can be supported by the two wires AB
and AC. The working stresses are 100 MPa for AB and 150 MPa for AC. The cross-
sectional areas of AB and AC are 400 mm² and 200 mm2, respectively.
B
30°
45°
FIG. P1.3
PROB. 1. For the truss shown in Fig. 1, Calculate the
stresses in members CE, DE and DF. The
cross-sectional area of each member is 1500 mm²
2.0 M
B
с
1.5M
4⁰ KN
Fig. 1,
2.0 m
E
IS M
D 2.0 m
50 KN
F
A doubly symmetrical I-section beam is reinforced by a flat plate attached to the upper flange as
shown in Fig. P.10.3. If the resulting compound beam is subjected to a vertical shear load of
200 kN, determine the distribution of shear stress in the portion of the cross section that extends
from the top of the plate to the ncutral axis. Calculate also the shcar force per unit length of bcam
resisted by the shear connection between the plate and the flange of the I-section beam.
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- Prob. 1.4-15. Determine the internal resultants FG, VG, and Me on the cross section at G of the horizontal frame member in Fig. P1.4-15. The uniformly distributed load on member AC has a magnitude w, = 3.2 kN/m. (See the inset for a definition of the resultants.) 60° B 1 m G B 0.5 m 0.5 m MG VG FG G P1.4-15 and P2.2-16 WO CIT 1.2 m D-+ 0.6 marrow_forwardPROB. 1. For the truss shown in Fig. 1, Calculate the stresses in members CE, DE and DF. The cross-sectional area of each member is 1500 mm² A 2.0 M B C 1.5M 4⁰ KN Fig. 1, 2.0 m E (1) 1.SM D 2.0 m 50 KN Farrow_forwardQuestion 5 (a) The beam has the rectangular cross section shown in the Fig. Q5(a). i) Determine the largest load P that can be supported on its overhanging ends so that the bending stress does not exceed o = 10MPa. max Point A is located at the left support section at a distance 100mm from the top face of the beam. If P = 12kN, calculate the normal stress and shearing stress at point A. Using the Mohr's circle method to determine the principal stresses and the maximum shearing stress at point A. 1.5 m -1.5 m Fig. Q5(a) 1.5 m OP 150 mm 250 mmarrow_forward
- iss 40 mm 200 m 40 mm FIG. P5.100 5.100 The bending moment acting on the cross section of the beam is M = 1.8 kN m. Find the maximum tensile and compressive bending stresses acting on the cross section.arrow_forward9.9. A curved beam with a rectangular cross section strikes a 90° arc and is loaded and supported as shown in Fig. P9.9. The thickness of the beam is 50 mm. Determine the hoop stress along line A-A at the inside and out- side radii and at the centroid of the beam. 45° 200 KN Figure P9.9 500 mm 500 mmarrow_forwardA cast iron beam is of T-section as shown in Fig. 7.21. The beam is şimply supported on a span of 8 m. The beam carries a uniformly distributed load of 1.5 kN/m length on the entire span. Determine the maximum tensile and maximum compressive stresses. 100 mm 20 mm 32.23 Fmm 80 mm 100 mm 67.77 mm 20 mm- Fig. 7.21arrow_forward
- Prob.2 Determine (a) the maximum bending stress, (b) the maximum shearing stress due to V in the simply supported beam shown in the figure and (c) the shearing stress at a point 1m from the right support and 2 cm below the top. 40 kN/m 5 сm 16 kN m 16 cm - 1m- - 2 m - 2 m-arrow_forward0.5 in. B 1.8 in. C Fig. P1.60 1.61 For the assembly and loading of Prob. 1.60, determine (a) the average shearing stress in the pin at C, (b) the average bearing stress at C in member BC, (c) the average bearing stress at B in member BC. 5 kips 5 kips 0.5 in. 1.8 in.arrow_forwardQ3/1.Determine the type of the truss in Fig.(3) 2.If the truss is made of a material has maximum allowable force 2.5KN in tension and 1.75KN in compression, determine the largest load P that can be applied to that truss. 1.5m - 3.6 m - Fig. (3) Barrow_forward
- Prob. 2.2-14. The three-member frame structure in Fig. P2.2-14 is subjected to a downward vertical load P at pin C. The pins at B, C, and D apply axial loads to members BD and CD, whose cross-sectional areas are A = 0.5 in² and A2 = 1.0 in², respectively. (a) If the axial stress in member BD is o = 1200 psi, what is the value of force P? (b) What is the corresponding axial stress, 02, in member CD? - 12 in.→|-- 12 in.- 9 in. B 9 in. C (1), 32 in. P (2) Darrow_forward1. Determine the reactions and the force in each member of the truss shown in Fig. below by the method of consistent deformations. -3 panels at 4 m 12 m- A (38 cm) B (38 cm) C 38 cm?) p 3m 20 KN (38 cm) F E=2 x 10 MPa 90 KN (38 cm Q5 cm) (38 cm)arrow_forward6.13 Determine the force in each member of the roof truss shown. State whether each member is in tension (T) or compression (C). 6 m -6 m 6 m 1.2 kN 2.4 kN F 2.4 kN D 1.2 kN 7.5 m B E 9 m 9 m Fig. P6.13arrow_forward
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