A support rod for the landing gear of a private airplane is subjected to a tensile load during landing. The loads are predicted to be as high as 40,000 pounds. Because the rod is crucial and failure could lead to a loss of life, the rod is to be designed with a factor of safety of 4 (that is, designed so that the rod is capable of supporting loads four times as great as expected). The operation of the system also produces loads that may induce cracks in the rod. Our non-destructive testing equipment can detect any crack greater than 0.02 in. deep. Based on the materials given in the following Table 7-1, design the support rod and the material, and justify your answer.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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A support rod for the landing gear of a private airplane is subjected to a tensile load during landing. The loads are predicted to be as high as 40,000 pounds. Because the rod is crucial and failure could lead to a loss of life, the rod is to be designed with a factor of safety of 4 (that is, designed so that the rod is capable of supporting loads four times as great as expected). The operation of the system also produces loads that may induce cracks in the rod. Our non-destructive testing equipment can detect any crack greater than 0.02 in. deep. Based on the materials given in the following Table 7-1, design the support rod and the material, and justify your answer.

TABLE 7-1 I The plane strain fracture toughness Kyc of selected materials
Fracture Toughness Kıc
(MPa /m)
Yield Strength or
Ultimate Strength (for Brittle Solids)
(МPа)
Material
Al-Cu alloy
24.2
455.1
36.3
324.1
Ti-6% Al-4% V
54.9
896.4
98.9
861.9
Ni-Cr steel
50.3
1641.0
87.9
1420.4
1.8
Al203
Si3N4
Transformation toughened ZrO2
Si3N4-SiC composite
Polymethyl methacrylate polymer
Polycarbonate polymer
206.9
4.9
551.6
11.0
413.7
56.0
827.4
1.0
27.6
3.3
57.9
Transcribed Image Text:TABLE 7-1 I The plane strain fracture toughness Kyc of selected materials Fracture Toughness Kıc (MPa /m) Yield Strength or Ultimate Strength (for Brittle Solids) (МPа) Material Al-Cu alloy 24.2 455.1 36.3 324.1 Ti-6% Al-4% V 54.9 896.4 98.9 861.9 Ni-Cr steel 50.3 1641.0 87.9 1420.4 1.8 Al203 Si3N4 Transformation toughened ZrO2 Si3N4-SiC composite Polymethyl methacrylate polymer Polycarbonate polymer 206.9 4.9 551.6 11.0 413.7 56.0 827.4 1.0 27.6 3.3 57.9
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