ca3_f23

I need to find the forces in each tube but I keep getting stuck. I have been getting really long equations to do algibra onwhich I suspect might be where the error was comming from. The values I have tried are F2 = -0.97786, and -4.889 kips

pls find box ur answer Determine the value of the von Mises stress at point A. The von Mises stress at point A is This problem illustrates that the factor of safety for a machine element depends on the particular point selected for analysis. Here you are to compute factors of safety, based upon the distortion-energy theory, for stress elements at A and B of the member shown in the figure. This bar is made of AISI 1006 cold- drawn steel and is loaded by the forces F= 0.55 kN, P = 4 kN, and T = 25 N-m. Given: Sy= 280 MPa. 5 15-mm D. 100 mm- MPa.

Please use ANSYS SOFTWARE

Needs Complete typed solution with 100 % accuracy.    Don't use chat gpt or ai i definitely upvote you.   Be careful Downvote for ai or chat gpt answer.

can you anser this question using figure 1? thank you.

Needs Complete typed solution with 100 % accuracy.         Don't use chat gpt or ai i definitely upvote you.

please wright by hand

Figure 1 shows a rotating shaft simply supported in ball bearings at A and D and loaded by a nonrotating force F of 6.8 kN. The shaft is machined from AISI 1050 cold-drawn steel. Estimate the life of the part. A 250 - 10 32 30 B 6.8 kN с D 75 100 125 10- 35 38 30 R₁₂ Figure 1. Shaft drawing showing all dimensions in millimeters; all fillets 3-mm radius A MB B M max Mc C D Figure 2. Bending-moment diagram

Please help with all need items, analysis, element, mohir circle, wtc. Thank you.

Solve 5,6

After recording the applied twisting moment and resulted angle, fill the following table MT (N.m) T. MPa (degree) (rad.) Now, the twisting moment-twisting angle and shear stress-shear strain curves can be plotted, then determine maximum shear stress, shear stress at proportional limit and modulus of rigidity. 4-6 Problem The following torsion test data were obtained for AA6061-T6 aluminum alloy has a round cross section with 30mm outer diameter, 0 inner diameter and 100 length. 0 32 130 Twisted angle (): 0 1 Torque (N.m): 286 347 487 5.5 591 786 910 1105 1163 1235 1222 3.5 6.5 7.5 9. 10.5 13.5 16.5 21.5 25.5 > Plot the torque-twisted angle curve and determine the proportional limit on it. Plot the shear stress-strain curve the determine the shearing strength and modulus of rigidity. Prof. Adnan N. Abood Asst. Lec. Zainah Waheed 25

Answer the problem with detailed step by step solution refer to the table of equations when answering the problem.

The state of stress at a point in an engine piston is given in the x-y-z coordinates by: 90 180 [0]=0, MPa = 180 240 yx yy 120 zy Using the matrix transformation law, determine the state of stress at the same point for an element rotated about the x-axis (in the y-z plane) 60° clockwise from its original position. Calculate the stress invariants and write the characteristic equation for the original state of stress, Calculate the deviatoric invariants for the original state of stress, Calculate the principal stresses and the absolute maximum shear stress at the point. What are the stress invariants and the characteristic equation for the transformed state of stress, а. b. С. d. e

Please complete the following with full workings. :)

Q4/a- Astructural component of an engineering design loaded in plane strain cnodition must support 250 MPa in tension. If the aluminium alloy AA7075-T6 is used for this application, calculate the length of the largest internal flaw that this material can support. Alloy Temper Proof Shear Elongation Hardness Kic (10 M) Tensile Stress Strength Strength (%) 0.2% (MPa) (MPa) Vickers (HV) Fatigue Strength 1/2 MPam (MPa) (MPa) AA7075 T6 503 572 331 11 175 25 159

Solve this Carefully, Write clearly and Circle the Final answer for Tmax with the correct units and for Part B T = with the right units

Compute Sn and sketch the goodman failure line for the part drawn below. Material is cold rolled steel. = 5 mm din' 10 mm 520 Mia Su 350 Men Raiobility= 90r こ Sa Sketch Goodman Failure line

Plz solve within 30min I vill give definitely upvote and vill give positive feedback thank you

Problem Set – Temperature Change 1. A steel tire has a dimensions indicated in the figure below. At 78 degrees Celsius, the said tire was fit into a 1.8m to an engine wheel with 24 degrees Celsius. Calculate the contact pressure between the tire and the wheel after fitting together due to colling of 24 degrees Celsius. The coefficient of expansion due to temperature of the tire is 12.3 micrometer/ m- degrees Celsius and Modulus of Elasticity is EN GPa. | 12 mm | 200 mm 900mm wide steel tire- 12 mm Note: Neglect the deformation of the wheel due to the pressure of the tire Fn- 100

Give me correct answer please someone give me wrong solve by hand

please written solution by hand

1-69.M Figure P1-69 shows a bolt subjected to a tensile load. One failure mode would be if the circular shank of the bolt pulled out from the head, a shearing action. Compute the shear stress in the head for this mode of failure if a force of 22.3 kN is applied. Applied force Shear area Reaction force on underside of head Cylindrical shear area 19.0 mm 8.00 mm -12.0 mm M12 x 1.75 thread

Could you plz complete qustions 4&5

URGENT

parts c-e please

At A, B, C and E there is a pin and at D a short wire. Determine By When solving the question please: 1)Free-Body diagram Clearly 2)dentify the data and constraints of the problem correct units 3)Equations used to solve the problem No big text just data

Perform a static stress analysis with linear material models on the problem shown in Figure 1 utilizing different mesh densities. Use meshes of 200, 400, 800, and 1600 elements. The thickness of the part given below is 8mm. A load of n MPa is applied on the right edge, where n is the last three digits of your UWE ID number. (for instance, for student 14020174, n is 174). The left end is fully fixed. Material is stainless steel (AISI 302) cold rolled. Assume it as a plane stress problem. Calculate stress concentration factor and compare with that of given in mechanics textbook. Write your comments in comparison with analytical solution. UFMFU7-15-3 Page 2 of 6 Radius =10 mm Fixed BC L. 40 mm 200 mm Figure 1

Define with absolute figure solve it correctly

please i need her solving and the final right answer quicklyy please

I need the full code of MATLAB

Strain and Stress equilibrium problems Please do create a free body diagram

Problem 2.33

Suppose that the assembled stiffness matrix of question 1 (as shown below) is as follows: [K]=108×a-a0-aa+b-b0-bb   where a=4.06 N/m and b=2.28 N/m. If the applied force at node 3 is P=210 KN, find the displacement of node 2 in mm?