The assembly has the diameters and material make-upindicated. It fits securely between its fixed supports whenthe temperature is T₁ = 70°F.(Figure 1)this is all the information given.Figure2014-T6 Aluminum12 in.-C 86100 Bronze8 in.6 ft304 Stainlesssteel-C₁ 4 in.3 ft1 of 1Part ADetermine the average normal stress in the aluminum when the temperature reaches T₂ = 124 °F.Express your answer to three significant figures and include the appropriate units.σal =SubmitPart BTheSubmitPart CDetermine the average normal stress in the bronze when the temperature reaches T₂ = 124 °F.Express your answer to three significant figures and include the appropriate units.TytHAValueSubmitRequest AnswerμÃValueRequest AnswerValueUnitsDetermine the average normal stress in the stainless steel when the temperature reaches T₂ = 124 °F.Express your answer to three significant figures and include the appropriate units.Request AnswerUnits?www ?Units?

To Find : The average normal stress in the aluminum. Given : The initial temperature is T1=70°F The…

The assembly has the diameters and material make-up indicated. It fits securely between its fixed supports when the temperature is T₁ = 70°F. (Figure 1) this is all the information given. Figure 2014-T6 Aluminum 12 in. 4 ft -C 86100 Bronze 8 in. 6 ft- 304 Stainless steel C₁ 4in. 1 of 1 Part A Determine the average normal stress in the aluminum when the temperature reaches T₂ = 124 °F. Express your answer to three significant figures and include the appropriate units. Tal = Submit Part B The = Submit Part C HA Value Request Answer Determine the average normal stress in the bronze when the temperature reaches T₂ = 124 °F. Express your answer to three significant figures and include the appropriate units. Value μÃ Request Answer HA st= Value Units Units Determine the average normal stress in the stainless steel when the temperature reaches T₂ = 124 °F. Express your answer to three significant figures and include the appropriate units. ? Units ? ?

The assembly has the diameters and material make-up indicated. It fits securely between its fixed supports when the temperature is T₁ = 70°F. (Figure 1) this is all the information given. Figure 2014-T6 Aluminum 12 in. 4 ft -C 86100 Bronze 8 in. 6 ft- 304 Stainless steel C₁ 4in. 1 of 1 Part A Determine the average normal stress in the aluminum when the temperature reaches T₂ = 124 °F. Express your answer to three significant figures and include the appropriate units. Tal = Submit Part B The = Submit Part C HA Value Request Answer Determine the average normal stress in the bronze when the temperature reaches T₂ = 124 °F. Express your answer to three significant figures and include the appropriate units. Value μÃ Request Answer HA st= Value Units Units Determine the average normal stress in the stainless steel when the temperature reaches T₂ = 124 °F. Express your answer to three significant figures and include the appropriate units. ? Units ? ?

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

See similar textbooks

Similar questions

The rod has a diameter of 40 mm. (Figure 1) It is subjected to the force system F = 1390 N, Fy = 510 N, F₂ = 835 N. Figure 5 300 mm 100 N-m F₂ 100 mm B 1 of 1 Determine the normal stress that acts at point B. Express your answer to three significant figures and include appropriate units. OB = Submit Part B (TB)xy 0 = μÅ Value Request Answer Determine the shear stress Try that acts at point B. Express your answer to three significant figures and include appropriate units. 0 μᾶ Units Value ? Units ?
-Which of the following statement/s is NOT true?Strain is dimensionlessThe cross-sectional area affected by the rivets in a plate is πdtStrain is the total deformation of the body divided by its original length.Shear stress is directed parallel to the area upon which it acts. -Which statement is NOT true about ksi? *Kilo (psi).1000 lb1 x10^3 psi.1 x10^3 lb. -Tensile stresses and strain are considered:negative tensile stress and positive lengthnegative increase in lengthpositive increase in lengthpositive tensile stress and negative length
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
1. Define the terms load , stress and strain. Discuss the various types of stresses and strain. 2. What is the difference between modulus of elasticity and modulus of rigidity? 3. Explain clearly the bearing stress developed at the area of contact between two members. 4. What useful informations are obtained from the tensile test of a ductile material? 5. What do you mean by factor of safety? 6. List the important factors that influence the magnitude of factor of safety. What is meant by working stress and how it is calculated from the ultimate stress or yield stress of a material? What will be the factor of safety in each case for different types of loading? 8. Describe the procedure for finding out the stresses in a composite bar. 7. 9. Explain the difference between linear and lateral strain. 10. Define the following: (a) Poisson's ratio, (b) Volumetric strain, and (c) Bulk modulus 11. Derive an expression for the impact stress induced due to a falling load. 12. Write short notes on…
The steel bar has the dimensions shown. (Figure 1) Figure 30 mm 24 mm- 20 mm co 60 mm r = 15 mm 1 of 1 Part A Determine the maximum axial force P that can be applied so as not to exceed an allowable tensile stress of allow = 160 MPa. Express your answer to three significant figures and include the appropriate units. P= Value Submit μA Provide Feedback 3 Request Answer Units ?
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.
DATE: A 01. The member consists of the steel rod AB that is screwed into the end of the bronze rod BC. Find the largest value of P that meets the following design criteria: (a) the overall length of the member is not to change by more than 3 mm; and (b) the stresses are not to exceed 140 MPa in steel and 120 MPa in bronze. The moduli of elasticity Steel A = 480 mm2 1.0 m |B 3P Bronze are 200 GPa for steel and 80 GPa for bronze. 2 m A = 650 mm? 2P
The rod has a diameter of 40 mm. (Figure 1) It is subjected to the force system F₂ = 1410 N, Fy = 635 N, F₂ - 820 N. Figure F F 300 mm 100 N-m F. 100 mm B 1 of 1 Determine the normal stress that acts at point B. Express your answer to three significant figures and include appropriate units. ов - Submit Part B (TB)zy μA Submit Value Request Answer Determine the shear stress Try that acts at point B. Express your answer to three significant figures and include appropriate units. BLA Value Request Answer Units ļ 20011 Units COOL ? HEIT
gure 1 shows a compound bar with three different diameters, d1-9mm, d2-22mm, and d3-14mm machined from solid aluminium alloy stock, subjected to a tensile load of 30kN. If Young's odulus for the alloy is 69GPA determine the stress in section 2. Answer to be provided in MPa, correct to three decimal places - do not include a unit with your answer. L1 L2 L3 d2 d3 P Figure 1
The tank of the air compressor is subjected to an internal pressure of 0.43 MPa as shown in (Figure 1). The internal diameter of the tank is 550 mm, and the wall thickness is 6 mm. Figure ⁹-1 Y Y Part A Determine the hoop stress acting at point A. Express your answer to three significant figures and include the appropriate units. 0 = Submit Part B 02 = Submit O Provide Feedback HA Value Request Answer Determine the longitudinal stress acting at point A. Express your answer to three significant figures and include the appropriate units. Value HÅ 1 h Units Request Answer Units ? F ?
The bar is made from steel and has an allowable stress of allow = 19.7 ksi (Figure 1) Figure 1.875 in. 0.75 in. 0.125 in. 1.25 in. r 0.25 in. 1 of 1 > Part A Determine the maximum axial force P that can be applied to the bar. Express your answer to three significant figures and include the appropriate units. μÃ P= 19.7 kips Submit Previous Answers Request Answer < Return to Assignment * Incorrect; Try Again; 2 attempts remaining ? Provide Feedback
Question 1 The normal stresses acting on element using standard sign conventions for stress ar are known to be o, = -96.2 MPa, o, = -19.3 MPa. The maximum shear stress is also to be tmax = 45.7 MPa. Considering the above system, determine the following information: 1.1 Shear stress acting on element, 1.2 The principal angle, 1.3 The principal stresses.