Answered You can hire a professional tutor to get the answer.
( 20 pts ) Consider a member made of 2024 - 14 aluminum (vield strength 325 MPa, ultimate strength 470 MPa) if the fully- reversed S- N diagram is...
Consider a member made of 2024-T4 aluminum (yield strength 325 MPa, ultimate strength 470 MPa) if the fully-reversed S-N diagram is represented as . 839 [ ] 0.102 N MPa a f− σ = At a location of interest the material is repeatedly subjected to the uniaxial stress history shown in the figure below. Estimate the number of repetitions of this loading history necessary to cause fatigue failure using the Palmgren-Miner rule.• Think carefully how the cycles in the "repetition" should be counted. Tabulate the mean stress, stress amplitude, number of cycles for each cycle type, and number of cycles to failure Nf for each type of cycle contained in the operational cycle.• Analyze your results and comment. Which portions of the loading history
3. ( 20 pts ) Consider a member made of 2024 - 14 aluminum (vield strength 325 MPa, ultimatestrength 470 MPa) if the fully- reversed S- N diagram is represented as . = $39 1 ,^ [MPallAt a location of interest the material is repeatedly subjected to the uniaxial stress history shownin the figure below . Estimate the number of repetitions of this loading history necessary tocause fatigue failure using the Palmgren - Miner rule .Think carefully how the cycles in the" repetition " should be counted . Tabulate the meanstress , stress amplitude , number of cycles for each cycle type , and number of cycles tofailure NE for each type of cycle contained in the operational cycle .`Analyze your results and comment . Which portions of the loading history mostcontribute to the fatigue failure of the part ?'275` [ MPQ] 2001001 2 0 0 0 9gg ( 1, 000 )END- 100time3 .0 0 9 10K_ ONE OPERATIONAL CYCLE -")( 10 pts ) GLARE is an example of a"Fiber - metal laminate" a combination of layers ofluminum and fiber composites made into a single composite .