e (C)d (mm)P(kN) Q(N)Gallow (MPa) s(%)20188012401(a)The structure shown in Figure Q3 is subjected to two point loads as shown. Determine(i)the axial force in rod BC and the reactions at pin A in terms of P. The value ofangle, 0 is given in Table 3.the maximum load, P that can be applied if the average shear stress in each(ii)pin is not allowed to exceed 60 MPa. All pins are subjected to double shearand each has a diameter, d as given in Table Q3. (Hint: Consider only pin Aand pin B.)RB2 m-+-2 mPPFigure Q3(b)A nylon thread is to be subjected to tension of Q (N). The modulus of elasticity, E ofthe thread is 3.2 GPa. Determine the required diameter of the thread, if(i)the maximum allowable normal stress is as given in Table 3;(ii)the length of the thread must not increase by more than s (%) as given inTable 3

Answered: Image /qna-images/answer/25807d6f-9e05-431c-a05d-aeb23abb7011.jpg

A nylon thread is to be subjected to tension of Q (N). The modulus of elasticity, E of the thread is 3.2 GPa. Determine the required diameter of the thread, if (i) the maximum allowable normal stress is as given in Table 3; the length of the thread must not increase by more than s (%) as given in (ii) Table 3

A nylon thread is to be subjected to tension of Q (N). The modulus of elasticity, E of the thread is 3.2 GPa. Determine the required diameter of the thread, if (i) the maximum allowable normal stress is as given in Table 3; the length of the thread must not increase by more than s (%) as given in (ii) Table 3

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Related questions

Q: An aluminum alloy cylinder with a diameter of 76 mm and a height of 150 mm. is subjected to a…

Q: 2. The tensile link shown is flat, is 5 mm. thick, and carries an axial loac a. Compute the maximum…

A: GIVEN- Axial load (P)=1350 N Thicknesss (t)= 5 mm

Q: An aluminum alloy [E = 67 GPa; v=0.33; a = 23.0 × 10-6/°C] plate is subjected to a tensile load P.…

Q: Problem 2: A bronze bar is fastened between a steel bar and an aluminum bar as shown. Axial loads…

A: Est=200GPa Eal=70GPa Ebr=83GPa Overall deformation= 3mm

Q: A beam of the cross section shown is made of a steel that is assumed to be elastoplastic with E= 200…

Q: Calculate Poisson's Ratio for a steel that has a modulus of elasticity E of 30,000,000 psi and a…

A: The given data is: Modulus of elasticity, E=30000000 psi Modulus of rigidity, G=11500000 psi

Q: The failure stress of a homogeneous steel bar having a diameter of 10 mm is 250 MPa. Using a factor…

Q: An extruded polymer beam is subjected to a bending moment M. The length of the bear is L = 500 mm.…

A: Given data Allowable tensile bendig stress = 18 MPa Allowable compressive bending stress = 9 MPa

Q: fracture. Determine the following for the two metals (show all calculations and units): a.…

A: Stress vs strain curve is given. BY doing matriculation we can find the unknown.

Q: An aluminum alloy [E = 72 GPa; v = 0.33; a= 23.0 x 10-6/°C] plate is subjected to a tensile load P.…

Question

e (C)
d (mm)
P(kN) Q(N)
Gallow (MPa) s(%)
20
18
80
12
40
1
(a)
The structure shown in Figure Q3 is subjected to two point loads as shown. Determine
(i)
the axial force in rod BC and the reactions at pin A in terms of P. The value of
angle, 0 is given in Table 3.
the maximum load, P that can be applied if the average shear stress in each
(ii)
pin is not allowed to exceed 60 MPa. All pins are subjected to double shear
and each has a diameter, d as given in Table Q3. (Hint: Consider only pin A
and pin B.)
RB
2 m-+-2 m
P
P
Figure Q3
(b)
A nylon thread is to be subjected to tension of Q (N). The modulus of elasticity, E of
the thread is 3.2 GPa. Determine the required diameter of the thread, if
(i)
the maximum allowable normal stress is as given in Table 3;
(ii)
the length of the thread must not increase by more than s (%) as given in
Table 3

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

SEE SOLUTION Check out a sample Q&A here

Step 1

Step 2

Step 3

Step 4

Step by step

Solved in 4 steps with 4 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, civil-engineering and related others by exploring similar questions and additional content below.

Similar questions

Part A An aluminum 2014-T4 alloy bar 2.50 inches wide and 0.750 inches in thickness has a 1/4 inch radius hole centered on its width, as shown in the sketch. With an axial load, P = 8650 lbs applied, the maximum axial stress at the edges of the hole was experimentally determined to be 7670 psi What is the stress concentration factor, K, of the hole? 1.33 0.75 1.66 1.50 P 2.50 in. -Radius 1/4 in. P= 8650 lbs
An aluminium wire (E=10,600 ksi) having a diameter d=1/8 inch. and length L=14 ft is subjected to a tensile load P. If the maximum permissible elongation of the wire is 1/6 inch and the allowable stress in tension is 10 ksi, what is the allowable load Pmax? Answer in Ibs
Calculate the stress and strain at each force interval. Plot a graph of the stress-strain curve. Estimate the yield point of the steel and note its location on the curve. Estimate the ultimate strength of the steel and note its location on the curve.
(b) (i) A tensile test specimen made from 0.4% C steel has a circular cross section of diameter d mm and a gauge length of 25 mm. When a load of 4500 N is applied during the test, the gauge length of the specimen extends to 25.02 mm. If the Young's Modulus of the steel is 199 GPa, calculate the diameter of the tensile test specimen used. 4
SITUATION. As shown in the figure below, a rigid bar with negligible mass is pinned at O and attached to two vertical rods. Assume that the rods were initially stress-free. Allowable stress in steel is 120 MPa and in bronze is 60 MPa. For this problem, a = 1.8m; b = 1.3m; c= 1.7m. a b C P Steel: A-900 mm² Bronze: A=1200 mm² E = 83 GPa L=2.0 m E = 200 GPa L=1.5m What is the value of P without exceeding the allowable stress of bronze, in kN? O 161 O 174 O 145 124 4
A steel component is subjected to alternate cyclical loading. The steel follows Basquin's law for high cycle fatigue, o, x N = C, (where the stress amplitude is in MPa). Ignore the geometric detail and assume that Marin's modifying factors are all equal to 1. You are given the minimum stress ain = -213 MPa, the maximum stress omax = 213 MPa. The material data are Tensile strength oUTS = 539 MPa, Basquin's constant c, = 875 MPa, Basquin's exponent a = 0.085. a) Calculate the stress ratio R, the stress amplitude o, in MPa and the mean stress am in MPa. The answers are acceptable with a tolerance of 0.01 for R and of 1 MPa the stresses. R: MPa MPа b) Calculate the corresponding life, in 10° cycles, (tolerance of 0.1 106 cycles) N :
A cylindrical specimen of some metal alloy having an elastic modulus of 101 GPa and an original cross-sectional diameter of 3.6 mm will experience only elastic deformation when a tensile load of 2430 N is applied. Calculate the maximum length of the specimen before deformation if the maximum allowable elongation is 0.41 mm. i mm
The solid rod has a diameter of 20mm. Find the following: Angle of twist at C with respect to A (in radians) Angle of twist at B with respect to A (in radians) Maximum shear stress at A (in MPa) (Shear stress at support, at a point 7mm from center. (in MPa) A-36 steel with the following properties: Modulus of Elasticity, E = 29x10^3 ksi or 200 GPa Shear Modulus/Modulus of Rigidity, G = 11.5x10^3 ksi or 79.3 GPa Poisson's Ratio, nu = 0.260 Temperature Coefficient for thermal expansion, a = 6.6x10^-6/°F or 11.7x10^-6/°C
X Your answer is incorrect. An extruded polymer beam is subjected to a bending moment M. The length of the beam is L = 620 mm. The cross-sectional dimensions of the beam are b1 = 39 mm, d1 = 82 mm, b2 = 23 mm, dɔ = 23 mm, and a = 8 mm. For this material, the allowable tensile bending stress is 20 MPa, and the allowable compressive bending stress is 12 MPa. Determine the largest moment M that can be applied as shown to the beam. b2 a d2 y A B b1 Answer: M = 412.360 N•m Attempts: 2 of 3 used
What is another term for bend? (A) flex B compress fracture D) twist E stretch