During a tension test, measurements for the applied load and the corresponding elongation are taken at frequent intervals. These data points are then used to:a. calculate the stress caused by the applied load at each data point.b. calculate the strain in the specimen induced by the applied load at each data point.c. plot a stress-strain diagram.d. all of the above

Shear stress is the force that tend to cause deformation of the material by sliding along the plane.…

During a tension test, measurements for the applied load and the corresponding elongation are taken at frequent intervals. These data points are a. calculate the stress caused by the applied load at each data point. b. calculate the strain in the specimen induced by the applied load at each data point.

During a tension test, measurements for the applied load and the corresponding elongation are taken at frequent intervals. These data points are a. calculate the stress caused by the applied load at each data point. b. calculate the strain in the specimen induced by the applied load at each data point.

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

Question: Principal stresses at a point are 80 N/mm2 and 40 N/mm² both tensile. The yield stress in simple tension for this material is 200 N/mm2 The values of factors of safety according to maximum principal stress theory and maximum shear stress theory, respectively, are
pls help me answer my homework. thank you.
Problem #2 (5 points): Fig. 2 shows aluminum hollow rods (outer diameter is 2 in. and inner diameter is 1.5 in.) that are fixed to rigid walls. The gap between the rods is 0.005 in when the temperature is 60°E. If the temperature is 200°F, what is the stress in each rod? aai = 13 x 10/F, Eai = 12 x 10 ksi %3D 0.005 in. .8 in. Fig. 2 Page | 1
The nominal stress-strain diagram for a specimen having an original diameter of 10 mm and a gauge length of 50 mm is shown below. Using the given nominal stress-nominal strain diagram, answer this question. The inset shows a detailed view of the curve at low strains. 400 350 300 250 Stress (MPa) 200 150 100 50 0 0.00 Stress (MPa) 350 kN 300 250 200 150 100 50 0 0.000 0.002 0.004 0.006 0.008 0.010 0.012 Strain 0.02 0.04 0.06 0.08 0.10 0.12 0.14 0.16 Strain 0.18 What is the maximum force that could be applied to the specimen before it plastically deforms?
Question- Principal stress at a point in an elastic material are 1.50 (tensile), o (tensile) and 0.50 (compressive). The elastic limit in tension is 210 MPa and poisson's ratio=0.3. Find the value of o at the failure when computed by the maximum principal strain theory.
Strength For the state of plane stress shown, determine the largest value of o, for which the maximum in plane shear stress is equal to or less than 75 MPa. After you determine the value, draw Mohr circle for the case
A 13 mm diameter tensile specimen has 50 mm gauge length. If the load corresponding to the 0.2% offset is 6800 kg, the yield stress will be nearly 1. 31 kg/mm² 2. 43 kg/mm² 3. 51 kg/mm² 4. 63 kg/mm² X
Give me right solution
650 600 550 500 450 400 350 300 250 200 150 100 50 0.002 0.004 0.006 0.008 0.01 0.012 0.014 0.016 0.018 0.02 Strain mm/mm The graph above shows the stress-strain relationship of a steel bar under tension test. The steel bar diameter = 8 mm and the bar gauge length = 100 mm. Determine the following: Toughness of the specimen Stress (MPa)
True or false
need help asap plsss tq....
difference between 1st principal stress, 2nd principal stress, and 3rd principal stress in mechaninical engineering