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nordsb [41]
3 years ago
12

A structural component in the shape of a flat plate 24.3 mm thick is to be fabricated from a metal alloy for which the yield str

ength and plane strain fracture toughness values are 533 MPa and 22.0 MPa-m1/2, respectively. For this particular geometry, the value of Y is 1.3. Assuming a design stress of 0.4 times the yield strength, calculate the critical length of a surface flaw.
Engineering
1 answer:
butalik [34]3 years ago
6 0

Answer:

the critical length of a surface flaw is 2.006x10⁻³m

Explanation:

the solution is attached in the Word file

Download docx
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Explanation:

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For a Cu-Ni alloy containing 53 wt.% Ni and 47 wt.% Cu at 1300°C, calculate the wt.% of the alloy that is solid and wt.% of allo
Zina [86]

Answer:

Hello your question is incomplete attached below is the complete question

answer: wt.% of alloy that is solid = 61.5%

             wt.% of allot that is liquid = 38.5%

Explanation:

To determine the wt.% of the alloy that is solid

= \frac{R}{R +S } * 100

=  \frac{53-45}{58-45} * 100  = 61.5%

To determine the wt.% of the alloy that is liquid

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attached below is a free hand sketch as well

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