The assembly has the diameters and material make-up indicated. It fitssecurely between its fixed supports when the temperature is 7₁-70"FEgurs.1)Figure2014-T6 Alumi12CM Br304sel1011Part ADetermine the average normal stress in the aluminum when the temperature reaches 75-106 "FExpress your answer to three significant figures and include the appropriate units.SubmitPart DHAValueX Incorrect, Try AgainoSustentPress Answers Reavest AnswDetermine the average normal stress in the bronze when the temperature reaches 7) 106 "FExpress your answer to three significant figures and include the appropriate units.0?HAUnitsValueUnits input for part AHearst AnswerUnitsPearson The assembly has the diameters and material make-up indicated. It fitssecurely between its fixed supports when the temperature is 7₁-70"FEgurs.1)Figure2014-T6 Alumi12CM Br304sel1011Part ADetermine the average normal stress in the aluminum when the temperature reaches 75-106 "FExpress your answer to three significant figures and include the appropriate units.SubmitPart DHAValueX Incorrect, Try AgainoSustentPress Answers Reavest AnswDetermine the average normal stress in the bronze when the temperature reaches 7) 106 "FExpress your answer to three significant figures and include the appropriate units.0?HAUnitsValueUnits input for part AHearst AnswerUnitsPearson

Answered: Image /qna-images/answer/caa049fa-b24b-4fc9-bbb0-f5e80c1b8d46.jpg

The assembly has the diameters and material make-up indicated. It fits securely between its fixed supports when the temperature is 7₁-70 "F Egurs 1) Figure 2014-T6 Alumi 32 CM B 304 sel 1 of 1 Part A Determine the average normal stress in the aluminum when the temperature reaches 75-106 "F Express your answer to three significant figures and include the appropriate units. Submit Part D HA Value X Incorrect, Try Again Sutent Press Answers Reavest Answ HA Units Determine the average normal stress in the bronze when the temperature reaches 7) 106 "F Express your answer to three significant figures and include the appropriate units. 0? Value Hearst Answer Units input for part A ? Units Pearson

The assembly has the diameters and material make-up indicated. It fits securely between its fixed supports when the temperature is 7₁-70 "F Egurs 1) Figure 2014-T6 Alumi 32 CM B 304 sel 1 of 1 Part A Determine the average normal stress in the aluminum when the temperature reaches 75-106 "F Express your answer to three significant figures and include the appropriate units. Submit Part D HA Value X Incorrect, Try Again Sutent Press Answers Reavest Answ HA Units Determine the average normal stress in the bronze when the temperature reaches 7) 106 "F Express your answer to three significant figures and include the appropriate units. 0? Value Hearst Answer Units input for part A ? Units Pearson

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

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The state of stress at a point in a member is shown on the element. Suppose that o = -40 MPa , oy = -120 MРа, три — -28 MPа . Part A Determine the normal stress component acting on the plane AB. (Figure 1) Express your answer with the appropriate units. HA ? Figure 1 of 1 Value Units Submit Request Answer Part B Determine the shear stress component acting on the plane A.B. 30% Express your answer with the appropriate units. y = | Value В Units Pearson
The state of stress at a point in a member is shown on the element. Suppose that o = -50 MPa , oy = -120 MPa , Try = -30 MPa Part A Determine the normal stress component acting on the plane AB. (Figure 1) Express your answer with the appropriate units. HA Value Units Submit Request Answer Figure 1 of 1 Part B A Determine the shear stress component acting on the plane AB. Express your answer with the appropriate units. 30% HA ? Tz'y = Value Units Submit Request Answer B
7. In the Brinell hardness test, if the load used 1200 kg, and the ball diameter 6 mm, write down the diameter of the indentation (in mm unit) if the BHN number was 586. * (1 Point) Enter your answer
pls help! Write the complete solutions and legibly. Answer in 2 decimal places. UPVOTE WILL BE GIVEN! MECHANICS OF DEFORMABLE BODIES Let Q = 0 and T = 8 (Example: 12Q°C = 120°C). Just substitute the number in letter. Thank you! Determine the normal stress and change in length of the aluminum rod if the temperature was raised by 12Q°C. The 0.5-mm gap exists at 2T°C.
Google Chrome attempt.php?attempt=514085&cmid%=103093&page=3 My bookmarks v es > ENGG1023-2020S2 > General > Assessment#2- Lab 曲 me Calendar Badges All courses A Brinell hardness measurement of 650 HBN, using a 10-mm-diameter indenter and a 2950 kg load on an aluminum plate, Determine the indentation diameter. O a. 2.683 mm O b. 2.836 mm O c. 2.368 mm Od. 2.386 mm Finish attempt search TOSHIBA F5 F6 F7 F8 F9 F10 F11 F12 & 15 6 7 01 7 V 9.
The rod has a diameter of 40 mm. (Figure 1) It is subjected to the force system Fx = 1170 N, Fy = 580 N, F₂ = 825 N. Figure 300 mm 100 N-m F₂ 100 mm 1 of 1 >
In the state of loading as made of brittle material tensile and compression fracture values of the exposed arm, respectively. σUT=200 MPa and σUC=800 MPa and factor of safety n=4 as it is; a) First reduce the applied forces to point B, b) By determining the critical point of the critical section and stresses Calculate it and show it on the stress element. c) Calculate the diameter of the AB part according to the Coulomb criterion. Note: Neglect the effect of cutting forces.
Tensile engineering stress-strain curves through failure are depicted below. Which specimen features the highest toughness? Engineering Stress, MPa 1800- 1600- 1400- 1200- 1000- 800- 600- 400- 200- Ol 0 Aluminum Alloy 2024-T81 0.04 0.08 Stainless Steel (18-8) 1340 Steel, Water-Quenched & Tempered at 370 C Magnesium 0.12 Structural Steel (Mild Steel) Engineering Strain 0.16 1340 Steel, Water-Quenched & Tempered at 370°C Aluminum Alloy 2024-T81 Structural Steel (Mild Steel) Stainless Steel (18-8) Magnesium 0.20 0.24
- Please select the correct answers according to the given figure for the elastic behaviour of steel and aluminium I. The elastic modulus of steel is about three times higher than the aluminum II. Aluminum deforms elastically three times as much as does steel III. Steel will show much smaller changes in dimensions IV. Steel is three times stiffer than the aluminum V. Aluminum is three times stiffer than the steel 50,000 40,000 Steel Aluminum 30,000 20,000 10,000 0. 0.001 0.002 0.003 0.004 0.005 Engineering strain e (in./in.) Engineering stress S (psi)
7. In the Brinell hardness test, if the load used 1200 kg, and the ball diameter 6 mm, write down the diameter of the indentation (in mm unit) if the BHN number was 586. * Enter your answer
The fluctuating stresses listed in the table are found at a critical location of a component made of steel with Se = 40 ksi, Sy = 80 ksi, Sut = 110 ksi and f= 0.87. These stresses are applied on the part within 10 s. What is the accumulative damage of this part? What is the life of the part in hours if this stress pattern continues to repeat for the remained of the part's life? Use Goodman criterion and Miner's rule in your solution. Loading order |Omin o max |Number of cycles -20 30 -10 50 1 3. -30 30 1
I Review Part A The rod has a diameter of 40 mm. (Figure 1) It is subjected to the force system F, = 1300 N, F, = 615 N, F = 910 N. Determine the normal stress that acts at point A. Express your answer to three significant figures and include appropriate units. HÀ ? OA = Value Units Submit Request Answer Figure < 1 of 1 Part B Determine the shear stress Try that acts at point A. 100 mm Express your answer to three significant figures and include appropriate units. 300 mm (TA)=y = Value Units 100 N-m Fy Submit Request Answer