Engineering, 01.03.2021 18:50 izabelllreyes
An aircraft component is fabricated from an aluminum alloy that has a plane strain fracture toughness of 32 . It has been determined that fracture results at a stress of 236 MPa when the maximum (or critical) internal crack length is 2.28 mm. (a) Determine the value of for this same component and alloy at a stress level of 354 MPa when the maximum internal crack length is 1.14 mm.
Answers: 3
Another question on Engineering
Engineering, 03.07.2019 15:10
Apiston-cylinder with a volume of 0.25 m3 holds 1 kg of air (r 0.287 k/kgk) at a temperature of 100 c. heat transfer to the cylinder causes an isothermal expansion of the piston until the volume triples. how much heat is added to the piston-cylinder?
Answers: 3
Engineering, 04.07.2019 18:20
Select any two (2) areas of applications of chain-drive. (clo4) a)-permanent lubrication necessary b)-hydraulic forklift truck operation c)-rigging and heavy moving materials d)-relatively high maintenance costs e)-costlier than belt drives
Answers: 2
Engineering, 04.07.2019 19:10
Arigid tank contains 10 kg of air at 137 kpa (abs) and 21°c. more air is added to the tank until the pressure and temperature rise to 242 kpa (abs) and 32°c, respectively. determine the amount of air added to the tank. [r-0.287 kj/kg k]
Answers: 3
Engineering, 04.07.2019 19:20
The process in which the system pressure remain constant is called a)-isobaric b)-isochoric c)-isolated d)-isothermal
Answers: 3
You know the right answer?
An aircraft component is fabricated from an aluminum alloy that has a plane strain fracture toughnes...
Questions
History, 29.09.2020 14:01
Mathematics, 29.09.2020 14:01
English, 29.09.2020 14:01
Mathematics, 29.09.2020 14:01
Mathematics, 29.09.2020 14:01
Mathematics, 29.09.2020 14:01
Mathematics, 29.09.2020 14:01
