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Do not copy else where they are wrong pls find what’s in yellow only

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.

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.

show all steps/solution

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

please solve with neat hand writing so I can understand

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

the question is attached in the image

solve, show all steps and fbd. do not provide copied answer or I will report      Do 12-15 using double integration.     (integration of moment)= theta, and integration of theta = v     mechanics of materials chapter 12

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

Answer the rest of the questions please

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

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

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

Calculate the Virtual Condition of the PIN in the drawing below: 1.000 O 1.000 .504 .982 C 1.008 2.000 Ø.995-1.000 +0.008MABC 6.00 O None of these answers is correct X 3.000 01.005-1.030 +0.005MABC B A .XX = .01 ANGLES= ± 1°

Do part b,c,d

Problem 2 refers to the following: a load P is applied to the cantilever beam shown which causes it to bend and deflect elastically: 2. a. b. 6 C. Gage 1 2 3 4 5 6 5 3 4 on bottom Strain (ue) A student group recorded the following strains from the loaded beam but failed to record which gages (1-6) the strain recordings came from (all strains are in microstrain): -154, 318, -23, 555,-323, 81. 2 1 Write the correct strain readings in the table above. Note gages 1, 3, 4, and 5 are longitudinal gages, and gages 2 and 6 are transverse gages. Gage 4 is on the bottom of the beam and is the same distance from the load as gage 3. Calculate an estimate of Poisson's ratio for this material. If the elastic modulus for this material is 10 Mpsi, calculate the uniaxial stress at the location of gages 5 & 6.

Need only handwritten solution only (not typed one).

Please solve, the value of n=2, thanks

Two 400 mm diameter pulleys are keyed to a simply supported shaft 500 mm apart. Each pulley is 100 mm from its support and has horizontal belts, tension ratio being 2.5. If the shear stress is to be limited to 80 MPa while transmitting 45 kW at 900 r.p.m., find the shaft diameter if it is to be used for the input-output belts being on the same or opposite sides. [Ans. 40 mm]

Please solve in detail. Don't use chatgpt,The Free body diagram must be drawn.