• Problem 2 Find the stresses and compressions in each section of the composite member shown below. • S a Use E = 30×10 psi, Eα = 107 psi, and the minimum number of bar elements. d = 2 in. d = 4 in. d = 2.5 in. 200 kips Steel Alum. Steel ти -12 in.. 8 in. ✓ -10 in. k = 1010 lb/in. S Steel, E = 30 × 106 psi Aluminum, E₁ = 10 × 106 psi kip = 103 lb a

• Problem 2 Find the stresses and compressions in each section of the composite member shown below. • S a Use E = 30×10 psi, Eα = 107 psi, and the minimum number of bar elements. d = 2 in. d = 4 in. d = 2.5 in. 200 kips Steel Alum. Steel ти -12 in.. 8 in. ✓ -10 in. k = 1010 lb/in. S Steel, E = 30 × 106 psi Aluminum, E₁ = 10 × 106 psi kip = 103 lb a

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

Correct answer is written below. Detailed and complete solution only. I will upvote, thank you.
A hollow aluminum cylinder made of 2014-T4 has an outside diameter of 2.50 in. and a wall thickness of 0.085 in. Its length is 14.5 in. What axial com- pressive force would cause the cylinder to shorten by 0.005 in.? What is the resulting stress in the 3-25. aluminum?
8.1 Please help ASAP. Provide Free Body Diagram, labeled with appropriate quantities to better understand. Also solve. Thank you.
Displacement with elemental stiffness method, the rest the same.
3. A steel bolt and nut are tightened around an aluminum sleeve. Find the internal forces as the nut is rotated 1 turn (1 turn = 1.5 mm) given the cross sectional areas and the moduli of elasticity for the steel and the aluminum. AST = 150 mm? EST = 200 GPa EAL = 70 GPa AAL = 100 mm? L=150 mm AST Final 1.5 mm Position Al
I need full details solution and please don't provide handwirrite solution.
2) A machine frame is made of steel having Sy = 400 MPa and Ssy = 250 MPa. When loaded in a test fixture, the stresses were found to vary linearly with load. Two points on the surface were found to be most critical. With a 4-kN test load, stresses at these points were: point a, 0₁ = 200 MPa, 0₂ = 100 MPa; point b, 0₁ = 150 MPa, 0₂ = -100 MPa. Compute the test load at which the frame will experience initial yielding according to the (a) maximum-normal-stress theory, (b) maximum-shear-stress theory, and (c) maximum-distortion-energy theory. Discuss briefly the relative validity of each theory for this application. Considering all the information available, what is your best judgment of the value of the test load at which yielding would actually be expected to begin? 02= 100 MPa a 02 02=-100 MPa b 02 0₁ = 200 MPa 01 = 150 MPa
I need both parts solution if u dont know both parts please skip if u give me right ans i surely gives u like
Pelase don't provide handwritten solution ....
Please Fast.
PROVIDE A CLEAR SOLUTION AND THE RIGHT ANSWER FOR THIS PROBLEM. PROVIDE INDIVIDUAL FBD
Need solution tnx