A rectangular rosette strain gage (Figure 2.20b) is cemented to the free surface of a machine part made of class 30, gray cast iron (Table A.1). In a test of the part, the following strains were recorded: ϵa = 0.00080, ϵb = 0.00010, and ϵc = 0.00040. Determine the stress components at the point on the surface with respect to the x–y axis shown.
FIGURE 2.20 Rosette strain gages. (a) Delta rosette. (b) Rectangular rosette.
TABLE A.1: Properties in S.I. Units
Material | Density [103 Kg/m3] | Yieldstress[MPa] | Ultimatestress[MPa] | Poisson’sratio | Young'smodulus[GPa] | Percent elongation at rupture | Thermal coefficient [10−6/°C] |
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STEEL | |||||||||||||
Structural, ASTM A36 | 7.85 | 250 | 400 | 0.29 | 200 | 30 | 11.7 | ||||||
AISI-C 1018, cold drawn | 7.85 | 370 | 440 | 0.29 | 200 | 15 | 11.7 | ||||||
AISl-C 1030, normalized | 7.85 | 340 | 530 | 0.29 | 200 | 30 | 11.7 | ||||||
AISI-C 1040, normalized | 7.85 | 390 | 590 | 0.29 | 200 | 28 | 11.7 | ||||||
AISI-C 1080, normalized | 7.85 | 520 | 1010 | 0.29 | 200 | 11 | 11.7 | ||||||
ASSI-3140, normalized | 7.85 | 620 | 900 | 0.29 | 200 | 19 | 11.7 | ||||||
AISI-4340, normalized | 7.8 | 860 | 1310 | 0.29 | 200 | 12 | 11.7 | ||||||
AISI 301 Stainless, annealed | 7.92 | 280 | 760 | 0.27 | 193 | 60 | 17.3 | ||||||
AISI 301 Stainless, half hard | 7.92 | 760 | 1030 | 0.27 | 193 | 15 | 17.3 | ||||||
CAST IRON | |||||||||||||
Gray, Class 30 (tension) | 7.21 | — | 210 | 0.20 | 103 | nil | 12.1 | ||||||
Gray, Class 30 (compression) | 7.21 | — | 510 | 0.20 | 103 | nil | 12.1 | ||||||
Gray, Class 40 (tension) | 7.21 | — | 410 | 0.20 | 138 | nil | 12.1 | ||||||
Gray, Class 40 (compression) | 7.21 | — | 990 | 0.20 | 138 | nil | 12.1 | ||||||
ALUMINUM ALLOYS | |||||||||||||
1100-H12 | 2.71 | 103 | 110 | 0.33 | 70.0 | 25 | 23.5 | ||||||
2024 T4 | 2.77 | 320 | 470 | 0.33 | 74.5 | 19 | 22.5 | ||||||
6061 T6 | 2.7 | 275 | 310 | 0.33 | 69.0 | 12 | 23.6 | ||||||
6063 T5 | 2.7 | 145 | 185 | 0.33 | 69.0 | 12 | 23.4 | ||||||
7075 T6 | 2.77 | 500 | 570 | 0.33 | 72.0 | 11 | 22.5 | ||||||
COPPER ALLOYS | |||||||||||||
Free-Cutting Copper, soft | 8.91 | 62 | 220 | 0.35 | 117 | 42 | 17.6 | ||||||
Free-Cutting Copper, hard | 8.91 | 290 | 320 | 0.35 | 117 | 12 | 17.6 | ||||||
Yellow Brass, annealed | 8.43 | 117 | 340 | 0.35 | 105 | 60 | 20.0 | ||||||
Yellow Brass, half hard | 8.43 | 340 | 420 | 0.35 | 105 | 23 | 20.0 | ||||||
Commercial Bronze, annealed | 8.84 | 90 | 270 | 0.35 | 110 | 45 | 18.0 | ||||||
Commercial Bronze, half hard | 8.84 | 280 | 330 | 0.35 | 110 | 25 | 18.0 | ||||||
TITANIUM |
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Alloy Ti–Al–V | 4.54 | 890 | 930 | 0.33 | 114 | 12 | 9.5 | ||||||
TIMBER (12% MC) | |||||||||||||
Coastal Douglas Fir (bending) | 0.48 | — | 85 | — | 13.4 | — | 3.1–4.5a | ||||||
Loblolly Pine (bending) | 0.51 | — | 88 | — | 12.3 | — | 3.1–4.5a | ||||||
White Oak (bending) | 0.68 | — | 105 | — | 12.3 | — | 3.1–4.5a | ||||||
CONCRETE | |||||||||||||
Medium Strength (compression) | 2.32 | — | 28 | 0.15 | 25.0 | — | 9.9 | ||||||
aParallel to the grain.
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