Engineering, 01.07.2020 20:01 bri9263

Calculate the maximum internal crack length allowable for a 2024-T3 aluminum alloy component that is loaded to a stress one-half of its yield strength. Assume a yield strength 345 MPa, a plane strain fracture toughness of 44 MPa and that Y

Answers: 2

Show answers

Other questions on the subject: Engineering

Engineering, 04.07.2019 18:10, lerasteidl

Determine whether or not it is possible to compress air adiabatically from k to 140 kpa and 400 k. what is the entropy change during this process?

Answers: 3

continue

Engineering, 04.07.2019 18:10, salazjlove

Which of the following refers to refers to how well the control system responds to sudden changes in the system. a)-transient regulation b)- distributed regulation c)-constant regulation d)-steady-state regulation

Answers: 1

continue

Engineering, 04.07.2019 18:20, ashleyjaslin

Derive the correction factor formula for conical nozzle i=-(1+ cosa) and calculate the nozzle angle correction factor for a nozzle whose divergence hal-fangle is 13 (hint: assume that all the mass flow originates at the apex of the cone.

Answers: 3

continue

Engineering, 04.07.2019 18:20, kodyclancy

Aquick transition of the operating speed of a shaft from its critical speed will whirl amplitude. (a) increase (b) limit (c) not affect (d) zero

Answers: 2

continue

You know the right answer?

Calculate the maximum internal crack length allowable for a 2024-T3 aluminum alloy component that is...