Introduction to Thread Tensile Stress Areas
The tensile stress area of a thread, often denoted as As, represents the effective cross-sectional area that bears the tensile load in threaded fasteners. This parameter is crucial in mechanical design for calculating the strength and load-bearing capacity of bolts, screws, and other threaded components. It accounts for the thread geometry and is derived from established industry standards such as GB/T 16823.1-1997 for metric threads and ASME B1.1 for unified inch threads.
In engineering applications, accurate knowledge of the stress area ensures safe and efficient designs, preventing failures under axial loads. This chart provides comprehensive data for both metric (ISO-based) and inch (Unified) threads, including various pitches and thread counts. Use this resource for structural analysis, fastener selection, and compliance with international standards.
- Metric threads are specified in millimeters, covering sizes from M1 to M70.
- Inch threads include UNC (coarse) and UNF (fine) series, from #1 to 3-3/4 inches.
- All values are verified against standard formulas to ensure reliability.
Metric Thread Tensile Stress Area Table (Units: mm)
The following table lists the nominal diameter, pitch (P), and tensile stress area (As in mm²) for metric threads. Data is sourced from GB/T 16823.1-1997, which defines stress and bearing areas for threaded fasteners. Note that for each diameter, multiple pitches are provided where applicable, reflecting coarse and fine thread options.
| Thread | Pitch P (mm) | Stress Area As (mm²) | Thread | Pitch P (mm) | Stress Area As (mm²) | Thread | Pitch P (mm) | Stress Area As (mm²) |
|---|---|---|---|---|---|---|---|---|
| M1 | 0.25 | 0.46 | M12 | 1.75 | 84.27 | M36 | 2 | 914.54 |
| M1 | 0.2 | 0.52 | M12 | 1.5 | 88.13 | M36 | 1.5 | 939.85 |
| M1.1 | 0.25 | 0.59 | M12 | 1.25 | 92.07 | M39 | 4 | 975.76 |
| M1.1 | 0.2 | 0.65 | M12 | 1 | 96.1 | M39 | 3 | 1028.39 |
| M1.2 | 0.25 | 0.73 | M14 | 2 | 115.44 | M39 | 2 | 1082.41 |
| M1.2 | 0.2 | 0.8 | M14 | 1.5 | 124.55 | M39 | 1.5 | 1109.94 |
| M1.4 | 0.3 | 0.98 | M14 | 1 | 134 | M42 | 4.5 | 1120.92 |
| M1.4 | 0.2 | 1.15 | M16 | 2 | 156.67 | M42 | 4 | 1148.93 |
| M1.6 | 0.35 | 1.27 | M16 | 1.5 | 167.25 | M42 | 3 | 1205.98 |
| M1.6 | 0.2 | 1.57 | M16 | 1 | 178.17 | M42 | 2 | 1264.42 |
| M1.8 | 0.35 | 1.7 | M18 | 2.5 | 192.47 | M45 | 4.5 | 1306.01 |
| M1.8 | 0.2 | 2.04 | M18 | 2 | 204.18 | M45 | 4 | 1336.23 |
| M2 | 0.4 | 2.07 | M18 | 1.5 | 216.24 | M45 | 3 | 1397.71 |
| M2 | 0.25 | 2.45 | M18 | 1 | 228.63 | M45 | 2 | 1460.57 |
| M2.2 | 0.45 | 2.48 | M20 | 2.5 | 244.8 | M48 | 5 | 1473.16 |
| M2.2 | 0.25 | 3.03 | M20 | 2 | 257.98 | M48 | 4 | 1537.67 |
| M2.5 | 0.45 | 3.39 | M20 | 1.5 | 271.5 | M48 | 3 | 1603.57 |
| M2.5 | 0.35 | 3.7 | M20 | 1 | 285.38 | M48 | 2 | 1670.85 |
| M3 | 0.5 | 5.03 | M22 | 2.5 | 303.4 | M52 | 5 | 1757.84 |
| M3 | 0.35 | 5.61 | M22 | 2 | 318.06 | M52 | 4 | 1828.25 |
| M3.5 | 0.6 | 6.78 | M22 | 1.5 | 333.06 | M52 | 3 | 1900.05 |
| M3.5 | 0.35 | 7.9 | M22 | 1 | 348.4 | M52 | 2 | 1973.22 |
| M4 | 0.7 | 8.78 | M24 | 3 | 352.51 | M70 | 6 | 3254.39 |
| M4 | 0.5 | 9.79 | M24 | 2 | 384.42 | M70 | 4 | 3446.88 |
| M4.5 | 0.75 | 11.32 | M24 | 1.5 | 400.89 | M70 | 3 | 3545.2 |
| M4.5 | 0.5 | 12.76 | M24 | 1 | 417.71 | M70 | 2 | 3644.9 |
| M5 | 0.8 | 14.18 | M27 | 3 | 459.41 | M70 | 1.5 | 3695.27 |
| M5 | 0.5 | 16.12 | M27 | 2 | 495.74 | |||
| M6 | 1 | 20.12 | M27 | 1.5 | 514.43 | |||
| M6 | 0.75 | 22.03 | M27 | 1 | 533.46 | |||
| M7 | 1 | 28.86 | M30 | 3.5 | 560.59 | |||
| M7 | 0.75 | 31.14 | M30 | 2 | 621.2 | |||
| M8 | 1.25 | 36.61 | M30 | 1.5 | 642.1 | |||
| M8 | 1 | 39.17 | M30 | 1 | 663.34 | |||
| M8 | 0.75 | 41.81 | M33 | 3.5 | 693.56 | |||
| M10 | 1.5 | 57.99 | M33 | 2 | 760.8 | |||
| M10 | 1.25 | 61.2 | M33 | 1.5 | 783.91 | |||
| M10 | 1 | 64.49 | M36 | 4 | 816.73 | |||
| M10 | 0.75 | 67.88 | M36 | 3 | 864.94 |
Calculation Formula for Metric Threads
The tensile stress area for metric threads is calculated using the formula:
As = (π / 4) × [(d₂ + d₃) / 2]²
Where:
- d₂: Basic pitch diameter of external thread (per GB/T 196).
- d₃: Minor diameter of external thread, calculated as d₃ = d₁ – H/6.
- d₁: Basic minor diameter of external thread (per GB/T 196).
- H: Fundamental triangle height (per GB/T 192).
This formula ensures precise computation for custom or non-standard threads, aligning with ISO 898-1 requirements for fastener strength.
Inch Thread Tensile Stress Area Table (Units: inch)
This table provides data for unified inch threads, including nominal diameter (d), size in inches, threads per inch (n), and tensile stress area (As in in²). It covers both UNC (coarse) and UNF (fine) series, based on ASME B1.1 standards.
| Nominal Diameter d | Size (inch) | Threads/n | Stress Area As (in²) | Nominal Diameter d | Size (inch) | Threads/n | Stress Area As (in²) |
|---|---|---|---|---|---|---|---|
| 1# | 0.073 | 64 | 0.00262 | 1# | 0.073 | 72 | 0.00278 |
| 2# | 0.086 | 56 | 0.0037 | 2# | 0.086 | 64 | 0.00393 |
| 3# | 0.099 | 48 | 0.00486 | 3# | 0.099 | 56 | 0.00523 |
| 4# | 0.112 | 40 | 0.00603 | 4# | 0.112 | 48 | 0.0066 |
| 5# | 0.125 | 40 | 0.00796 | 5# | 0.125 | 44 | 0.00831 |
| 6# | 0.138 | 32 | 0.00909 | 6# | 0.138 | 40 | 0.01014 |
| 8# | 0.164 | 32 | 0.01401 | 8# | 0.164 | 36 | 0.01473 |
| 10# | 0.1875 | 24 | 0.01695 | 10# | 0.1875 | 32 | 0.01937 |
| 12# | 0.216 | 24 | 0.02416 | 12# | 0.216 | 28 | 0.02579 |
| 1/4 | 0.25 | 20 | 0.03182 | 1/4 | 0.25 | 28 | 0.03637 |
| 5/16 | 0.3125 | 18 | 0.05243 | 5/16 | 0.3125 | 24 | 0.05807 |
| 3/8 | 0.375 | 16 | 0.07749 | 3/8 | 0.375 | 24 | 0.08783 |
| 7/16 | 0.4375 | 14 | 0.10631 | 7/16 | 0.4375 | 20 | 0.11872 |
| 1/2 | 0.5 | 13 | 0.1419 | 1/2 | 0.5 | 20 | 0.15995 |
| 9/16 | 0.5625 | 12 | 0.18194 | 9/16 | 0.5625 | 18 | 0.20298 |
| 5/8 | 0.625 | 11 | 0.226 | 5/8 | 0.625 | 18 | 0.25596 |
| 3/4 | 0.75 | 10 | 0.33446 | 3/4 | 0.75 | 16 | 0.37296 |
| 7/8 | 0.875 | 9 | 0.46173 | 7/8 | 0.875 | 14 | 0.50947 |
| 1 | 1 | 8 | 0.60575 | 1 | 1 | 12 | 0.66304 |
| 1-1/8 | 1.125 | 7 | 0.76328 | 1-1/8 | 1.125 | 12 | 0.85572 |
| 1-1/4 | 1.25 | 7 | 0.96911 | 1-1/4 | 1.25 | 12 | 1.07295 |
| 1-3/8 | 1.375 | 6 | 1.15488 | 1-3/8 | 1.375 | 12 | 1.31471 |
| 1-1/2 | 1.5 | 6 | 1.40525 | 1-1/2 | 1.5 | 12 | 1.58102 |
| 1-3/4 | 1.75 | 5 | 1.89946 | ||||
| 2 | 2 | 4.5 | 2.49823 | ||||
| 2-1/4 | 2.25 | 4.5 | 3.24769 | ||||
| 2-1/2 | 2.5 | 4 | 3.99883 | ||||
| 2-3/4 | 2.75 | 4 | 4.93401 | ||||
| 3 | 3 | 4 | 5.96737 | ||||
| 3-1/4 | 3.25 | 4 | 7.09891 | ||||
| 3-1/2 | 3.5 | 4 | 8.32862 | ||||
| 3-3/4 | 3.75 | 4 | 9.65651 |
Calculation Formula for Inch Threads
The tensile stress area for unified inch threads is calculated as:
As = 0.7854 × [d – (0.9743 / n)]²
Where:
- d: Nominal diameter in inches.
- n: Number of threads per inch.
This approximation derives from the effective diameter and is widely used in ASME and SAE standards for bolt strength calculations.
Applications and Importance in Mechanical Design
Tensile stress areas are essential for determining the allowable tensile load of threaded fasteners using the formula: F = As × σ, where σ is the material’s tensile strength. This aids in:
- Selecting appropriate bolt sizes for structural joints in automotive, aerospace, and construction industries.
- Ensuring compliance with safety factors in high-load applications like pressure vessels or machinery.
- Optimizing designs by comparing coarse vs. fine threads for fatigue resistance or assembly ease.
Always verify material properties and engagement lengths per relevant standards to avoid under- or over-design.
Usein kysytyt kysymykset (UKK)
- What is the difference between tensile stress area and minor diameter area?
- The tensile stress area (As) is an effective area accounting for thread root geometry, typically larger than the minor diameter area to reflect actual load distribution. It is used for strength calculations, while the minor diameter area is purely geometric.
- How does pitch affect the stress area in metric threads?
- Smaller pitches result in larger stress areas for the same diameter because they increase the effective diameter. For example, in M12, a 1 mm pitch yields As = 96.1 mm², compared to 84.27 mm² for 1.75 mm pitch.
- Are these values applicable to both bolts and screws?
- Yes, these stress areas apply to external threads on bolts and screws per GB/T 16823.1 and ASME B1.1, assuming standard thread forms. For internal threads, shear areas may differ.
- Why use fine threads over coarse ones?
- Fine threads provide higher stress areas and better fatigue resistance due to shallower roots, ideal for vibration-prone applications. However, coarse threads offer easier assembly and higher shear strength.
- How to calculate stress area for non-standard threads?
- Use the provided formulas with precise dimensions from GB/T 196 or ASME B1.1. For accuracy, measure d₂ and d₃ or consult software tools compliant with ISO 898-1.
- Is conversion between metric and inch systems straightforward?
- No, due to differing thread forms. Convert units (1 in² = 645.16 mm²), but select equivalent sizes based on load requirements, not direct dimensional match.
