Engineering, 05.05.2020 23:32 teagan56
11. Suppose that a wing component on an aircraft is fabricated from an aluminum alloy that has a plane strain fracture toughness of It has been determined that fracture results at a stress of 365 MPa (53,000 psi) when the maximum internal crack length is 2.5 mm (0.10 in.). For this same component and alloy, compute the stress level at which fracture will occur for a critical internal crack length of 4.0 mm (0.16 in.).
Answers: 1
Engineering, 03.07.2019 14:10, volleyballfun24
If the thermal strain developed in polyimide film during deposition is given as 0.0044. assume room temperature is kept at 17.3 c, and thermal coefficient of expansion for the film and the substrate are 54 x 10^-6c^-1 and 3.3 x 10^-6c^-1respectively. calculate the deposition temperature.
Answers: 3
Engineering, 04.07.2019 18:20, annette211pdd8v9
For a gate width of 2 m into the paper, determine the force required to hold the gate abc at its location.
Answers: 1
Engineering, 04.07.2019 19:10, Calliedevore
The proportional limit is always greater than the yield strength for a material. a)-trune b)- false
Answers: 3
11. Suppose that a wing component on an aircraft is fabricated from an aluminum alloy that has a pla...
History, 03.12.2019 22:31
Mathematics, 03.12.2019 22:31
History, 03.12.2019 22:31
Mathematics, 03.12.2019 22:31