For the beam in figure 1, find the value and location of the largest tensile and compressive stresses. There may be more than one candidate location for each of these. 3.2 kN/m 2 1.9 kN.m Im A 3m 2m Figure 1 Figure 2 The cross section shown in Figure 2 is 125x75x8 UA the cross section and material properties are shown below; (Note that in the tables, the horizontal and vertical coordinate n and p, and are right and up respectively. Table 26 Unequal Angles - x-axis and y-axis - Dimensions and Properties Designation Nominal Mass Actual Radii Thickness per Thickness About x-axis About y-axis Torsion Tan Designation Constant Alpha Gross Coordinate metre Area of of Centroid Cross Leg-size Root Toe (b,-t) (b,-t) Section b, x b, t r 5, t A Рап y Z V₁ mm mm mm ka/m mm mm mm mm² mm mm 10 mm mm 10 mm mm 125 x 75 x 12 UA 17.7 12.0 10 UA 14.2 9.5 8 UA 11.8 7.8 8.0 5.0 9.42 5.25 2260 8.0 5.0 12.2 6.89 1810 8.0 5.0 15.0 8.62 1500 43.3 18.4 42.3 17.5 3.20 41.5 16.8 2.68 3.91 83.2 83.8 84.2 59.7 31.8 Z Y₁ Z S r 10-mm³ mm 10 mm 10mm³ 47.0 65.5 34.6 113 81.4 41.6 38.2 59.3 53.9 33.9 94.4 65.8 58.9 45.5 33.3 80.4 54.6 V x, Z 2日 X mm 10 mm mm 0.585 19.9 42.0 0.476 19.2 42.2 0.399 18.6 10 mm³ mm 29.3 414 24.9 41.6 21.5 Z 10-mm³ mm 10 mm² 10mm 14.1 31.9 18.4 29.7 11.4 30.7 15.5 24.1 16.2 9.55 29.9 13.3 20.1 16.3 S r J mm 10 mm 16.1 110 0.356 125 x 75 x 12 UA 56.2 0.360 31.7 0.363 10 UA 8 UA Form Factor Table 27 Unequal Angles - x-axis and y-axis - Properties for Assessing Section Capacity Designation Yield Stress About x-axis About y-axis Yield Stress Form Factor About x-axis About y-axis Designation Load A Load C Load B Load D Load A f k₁ Z Z Z Z f k Z Load C Z Load B Z Load D Z mm mm mm MPa 10mm 10 mm 10'mm³ 10 mm MPa 10 mm 10 mm 10/mm³ 10-mm³ 300PLUS AS/NZS 3679.1-350 125 x 75 x 12 UA 300 1.00 68.6 70.5 20.6 21.2 340 1,00 67.6 70.5 20.3 21.2 125 x 75 x 12 UA 10 UA 320 1.00 51.6 572 15.5 17.2 360 1.00 50.6 57.2 15.2 17.2 10 UA 8 UA 320 0.964 39.8 46.0 119 14.3 360 0.931 38.8 44.7 11.6 14.3 8 UA Table 28 Unequal Angles - n-axis and p-axis - Dimensions and Properties Designation About n-axis About p-axis Product of 2nd Moment of Area Designation P Z P. Z S Z n₂ 6 mm mm mm 10 mm mm 10°mm³ mm 10 mm 10 mm mm 10 mm mm 10°mm³ mm 10'mm³ 10 mm mm 10 mm² 125 x 75 x 12 UA 3.54 43.3 818 81.7 43.3 77.3 39.6 0.958 18.4 52.0 56.6 16.9 31.4 20.6 -105 125 x 75 x 12 UA 10 UA 2.88 42.3 68.2 827 34.9 62.5 39.9 0.789 17.5 45.2 575 13.7 25.1 20.9 -0.867 10 UA 8 UA 2.41 415 58.1 83.5 28.9 52.0 40.1 0.664 16.8 39.6 58.2 114 20.7 21.0 -0.731 8 UA Value (MPa) Does this stress exceed the yield stress of the member? Location on beam (draw sketch) Location on Cross section (draw sketch) Largest tensile stress Largest compressive stress
For the beam in figure 1, find the value and location of the largest tensile and compressive stresses. There may be more than one candidate location for each of these. 3.2 kN/m 2 1.9 kN.m Im A 3m 2m Figure 1 Figure 2 The cross section shown in Figure 2 is 125x75x8 UA the cross section and material properties are shown below; (Note that in the tables, the horizontal and vertical coordinate n and p, and are right and up respectively. Table 26 Unequal Angles - x-axis and y-axis - Dimensions and Properties Designation Nominal Mass Actual Radii Thickness per Thickness About x-axis About y-axis Torsion Tan Designation Constant Alpha Gross Coordinate metre Area of of Centroid Cross Leg-size Root Toe (b,-t) (b,-t) Section b, x b, t r 5, t A Рап y Z V₁ mm mm mm ka/m mm mm mm mm² mm mm 10 mm mm 10 mm mm 125 x 75 x 12 UA 17.7 12.0 10 UA 14.2 9.5 8 UA 11.8 7.8 8.0 5.0 9.42 5.25 2260 8.0 5.0 12.2 6.89 1810 8.0 5.0 15.0 8.62 1500 43.3 18.4 42.3 17.5 3.20 41.5 16.8 2.68 3.91 83.2 83.8 84.2 59.7 31.8 Z Y₁ Z S r 10-mm³ mm 10 mm 10mm³ 47.0 65.5 34.6 113 81.4 41.6 38.2 59.3 53.9 33.9 94.4 65.8 58.9 45.5 33.3 80.4 54.6 V x, Z 2日 X mm 10 mm mm 0.585 19.9 42.0 0.476 19.2 42.2 0.399 18.6 10 mm³ mm 29.3 414 24.9 41.6 21.5 Z 10-mm³ mm 10 mm² 10mm 14.1 31.9 18.4 29.7 11.4 30.7 15.5 24.1 16.2 9.55 29.9 13.3 20.1 16.3 S r J mm 10 mm 16.1 110 0.356 125 x 75 x 12 UA 56.2 0.360 31.7 0.363 10 UA 8 UA Form Factor Table 27 Unequal Angles - x-axis and y-axis - Properties for Assessing Section Capacity Designation Yield Stress About x-axis About y-axis Yield Stress Form Factor About x-axis About y-axis Designation Load A Load C Load B Load D Load A f k₁ Z Z Z Z f k Z Load C Z Load B Z Load D Z mm mm mm MPa 10mm 10 mm 10'mm³ 10 mm MPa 10 mm 10 mm 10/mm³ 10-mm³ 300PLUS AS/NZS 3679.1-350 125 x 75 x 12 UA 300 1.00 68.6 70.5 20.6 21.2 340 1,00 67.6 70.5 20.3 21.2 125 x 75 x 12 UA 10 UA 320 1.00 51.6 572 15.5 17.2 360 1.00 50.6 57.2 15.2 17.2 10 UA 8 UA 320 0.964 39.8 46.0 119 14.3 360 0.931 38.8 44.7 11.6 14.3 8 UA Table 28 Unequal Angles - n-axis and p-axis - Dimensions and Properties Designation About n-axis About p-axis Product of 2nd Moment of Area Designation P Z P. Z S Z n₂ 6 mm mm mm 10 mm mm 10°mm³ mm 10 mm 10 mm mm 10 mm mm 10°mm³ mm 10'mm³ 10 mm mm 10 mm² 125 x 75 x 12 UA 3.54 43.3 818 81.7 43.3 77.3 39.6 0.958 18.4 52.0 56.6 16.9 31.4 20.6 -105 125 x 75 x 12 UA 10 UA 2.88 42.3 68.2 827 34.9 62.5 39.9 0.789 17.5 45.2 575 13.7 25.1 20.9 -0.867 10 UA 8 UA 2.41 415 58.1 83.5 28.9 52.0 40.1 0.664 16.8 39.6 58.2 114 20.7 21.0 -0.731 8 UA Value (MPa) Does this stress exceed the yield stress of the member? Location on beam (draw sketch) Location on Cross section (draw sketch) Largest tensile stress Largest compressive stress
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
Related questions
Question
Please answer the attached question which includes all the necessary background information sourced together for your convenience
AI-Generated Solution
AI-generated content may present inaccurate or offensive content that does not represent bartleby’s views.
Unlock instant AI solutions
Tap the button
to generate a solution
Recommended textbooks for you
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY