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Q4/a- Astructural component of an engineering design loaded in plane strain cnodition must support 250 MPa in tension. If the aluminium alloy AA7075-T6 is used for this application, calculate the length of the largest internal flaw that this material can support. Alloy Temper Proof Shear Elongation Hardness Kic (10 M) Tensile Stress Strength Strength (%) 0.2% (MPa) (MPa) Vickers (HV) Fatigue Strength 1/2 MPam (MPa) (MPa) AA7075 T6 503 572 331 11 175 25 159

Q4/a- Astructural component of an engineering design loaded in plane strain cnodition must support 250 MPa in tension. If the aluminium alloy AA7075-T6 is used for this application, calculate the length of the largest internal flaw that this material can support. Alloy Temper Proof Shear Elongation Hardness Kic (10 M) Tensile Stress Strength Strength (%) 0.2% (MPa) (MPa) Vickers (HV) Fatigue Strength 1/2 MPam (MPa) (MPa) AA7075 T6 503 572 331 11 175 25 159

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Q4/a- Astructural component of an engineering design loaded in plane strain cnodition must support 250 MPa in tension. If the aluminium alloy AA7075-T6 is used for this application, calculate the length of the largest internal flaw that this material can support. Alloy Temper Proof Shear Elongation Hardness Kic (10 M) Tensile Stress Strength Strength (%) 0.2% (MPa) (MPa) Vickers (HV) Fatigue Strength 1/2 MPam (MPa) (MPa) AA7075 T6 503 572 331 11 175 25 159
Transcribed Image Text:Q4/a- Astructural component of an engineering design loaded in plane strain cnodition must support 250 MPa in tension. If the aluminium alloy AA7075-T6 is used for this application, calculate the length of the largest internal flaw that this material can support. Alloy Temper Proof Shear Elongation Hardness Kic (10 M) Tensile Stress Strength Strength (%) 0.2% (MPa) (MPa) Vickers (HV) Fatigue Strength 1/2 MPam (MPa) (MPa) AA7075 T6 503 572 331 11 175 25 159
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