Engineering, 26.10.2021 18:40 rhussein6452
A wing component on an aircraft is fabricated from an aluminum alloy that has a plane strain fracture toughness of 23 . It has been determined that fracture results at a stress of 124 when the maximum internal crack length is 8.4 . For this same component and alloy, compute the stress level at which fracture will occur for a critical internal crack length of 5.8 .
Answers: 3
Engineering, 04.07.2019 18:20
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Engineering, 04.07.2019 18:20
Water vapor initially at 10 bar and 400 °c is contained within a piston-cylinder assembly. the water lost heat to the surrounding according to isochoric (iso-volumetric) process until its temperature is 150 °c. the water is then condensed isothermally to saturated liquid. for the water as a system, calculate the work in kj/kg
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Answers: 1
A wing component on an aircraft is fabricated from an aluminum alloy that has a plane strain fractur...
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