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Mechanical Properties

1/2 X 60-1/8 Carbon Steel, Deformed Bar Anchor
Material: C1008-C1018
Material Density US/metric: 0.284 / 0.00787
Spec: C1010
Standard: ASTM A496 / AWS D1.5 / AWS D1.1
Thread Class: N/A
Fastener: 1/2

Fastener Dimensional Properties

Nominal Diameter (in) Threads per Inch Calculated Pitch Diameter (in) Calculated Minor Diameter (in)
0.500 0.00 N/A N/A
Effective Weld Base Diameter Calculated Stress Area Full Body (in2) Calculated Stress Area Pitch (in2) Calculated Stress Area Threadsa (in2)
N/A 0.1963 N/A N/A

Material Properties

Ultimate Tensile Strength Minb (PSI)/(MPa) Yield Tensile Strength Minb (PSI)/(MPa) Proof Tensile Strength Minc (PSI)/(MPa)
90% YTM
Yield Shearing Stress Minc (PSI)/(MPa)
0.577*YTM
80,000 70,000 63,000 40,390

Thread Mechanical Properties

Tensile
Ultimate Tensile Strength Min UTM*SAT Yield Tensile Strength Min YTM*SAT Proof Load Tensile Strength PTM*SAT Preload Reused Tensiled
75% PL
Preload Permanente
90% PL
N/A N/A N/A N/A N/A
Torque Shear
Friction Coefficientf Torque Reused FC*PR*ND Torque Permanent FC*PP*ND Torque Ultimateg FC*UTS*ND Yield Shear Minh
YSM*SAT
N/A N/A N/A N/A N/A

Fastener Body Mechanical Properties

Tensile Shear
Full Diameter Yield Tensile Strength Min
YTM*SAF
Pitch Diameter Yield Tensile Strength Min
YTM*SAP
Full Diameter Yield Shear Min
YSM*SAF
Pitch Diameter Yield Shear Min
YSM*SAP
13,744 N/A 7,931 N/A
aStress area for the threads is calculated on an area approximately half way between the root diameter and pitch diameter. This more closely reflects actual results versus using root diameter for stress area calculations
bData provided by our suppliers
cProof Tensile is estimated to be 90% of Yield Tensile when Proof Tensile data is not readily available.
dPreload for reuse of threaded fastener is 75% of Proof Load. Fastener may be rebolted multiple times with no degradation.
ePreload for permanent installation of fastener is 90% of Proof Load. Fastener is permanently stretched and will not achieve the same clamping force on reuse.
fFriction Coefficient will vary greatly depending on bolting conditions including lubrication. 0.2 is standard when bolt condition is plain finish or unknown.
gUltimate Torque is not useful in designing a bolted joint. Preloaded torque is more practical. This data is provided as a reference only.
hUsing the distortion-energy theory; Maximum Shear Stress equals .577 times the Maximum Tensile.
Source: "Mechanical Engineering Design", 5th ed.; Shigley and Mischke, McGraw Hill, © 1989.

CAUTION: Fasteners should not be used at their tensile or shear limits. A safety factor must be applied to engineering calculations. The particular safety factor will vary depending on the application. Customers should always evaluate fasteners for suitability of their own applications.

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