A tap does not have to cut the full thread height. The tap drill sets how much of the theoretical sharp-V height the tap engages, and the standard shop practice is about 75%, which gives nearly the full strength of a 100% thread at roughly half the tapping torque. Going below 60% is common in tough materials like Inconel and titanium to save taps; going above 80% rarely adds strength and breaks taps.[1]
The calculator then picks the closest standard drill from the drill size chart and reports the percent of thread that drill actually gives, so you can see whether it landed slightly above or below your target.
A bolt in a tapped hole can fail three ways: the bolt breaks in tension, the bolt's external threads shear off, or the internal threads in the hole strip out. Good design makes the bolt break first, because a broken bolt is obvious and replaceable while stripped threads in a housing are neither. The engagement length that guarantees it comes from comparing the thread shear areas with the bolt's tensile stress area.[2]
| Quantity | Formula (basic dimensions, 60° threads) |
|---|---|
| Tensile stress area of the bolt | At = 0.7854 (D − 0.9743 / n)² inch, or 0.7854 (D − 0.9382 P)² metric |
| External thread shear area per unit length | As = π n Kn [1 / (2n) + 0.57735 (Es − Kn)], with Kn = D − 1.0825 P and Es = D − 0.6495 P |
| Internal thread shear area per unit length | An = π n Ds [1 / (2n) + 0.57735 (Ds − En)], with Ds = D and En = D − 0.6495 P |
| Engagement, equal materials | Le = 2 At / As (external thread shear area equal to twice the tensile area) |
| Correction for a weaker tapped material | J = (As × Ss,bolt) / (An × Ss,hole); if J > 1, multiply Le by J |
Shear strength is taken as 0.6 times tensile strength for every material in the tables, a common engineering approximation. The calculator uses basic thread dimensions; class 2A/2B allowances make the real shear areas a few percent smaller, so treat the result as a design minimum and round up to the next practical depth. It also assumes uniform load sharing along the engaged threads and does not cover thread inserts, fatigue, or fine-pitch threads in soft materials, which strip more easily than the areas suggest.
| Step | Value |
|---|---|
| Tap drill at 75%: 0.250 − 0.0130 × 75 / 20 | 0.2013 in → #7 drill (0.2010) |
| Tensile stress area At | 0.7854 × (0.250 − 0.0487)² = 0.0318 in² |
| Kn, Es | 0.1959 in, 0.2175 in |
| External shear area per inch As | π × 20 × 0.1959 × [0.025 + 0.57735 × 0.0217] = 0.462 in² per inch |
| Engagement for equal materials, 2 At / As | 0.0636 / 0.462 = 0.138 in (0.55 D) |
| Internal shear area per inch An | π × 20 × 0.250 × [0.025 + 0.57735 × 0.0325] = 0.687 in² per inch |
| J with Grade 5 (120 ksi) in 6061-T6 (45 ksi) | (0.462 × 72) / (0.687 × 27) = 1.79 |
| Minimum engagement in aluminum | 0.138 × 1.79 = 0.247 in, about 1.0 × D |
The result lands on the rule of thumb machinists already use, one diameter of engagement for a steel bolt in aluminum, and shows where it comes from. The same bolt in a 4140 pre-hard housing needs only the 0.14 in equal-material value, and in Delrin the multiplier climbs past 8, which is why plastic parts get threaded inserts.
Basic major diameters and pitches per ASME B1.1 (unified inch) and ISO 261 / ASME B1.13M (metric). The calculator reads this table when the page loads.[3]
| Series | Size | TPI (inch) or pitch (mm) | Major diameter (in or mm) |
|---|---|---|---|
| UNC | #1-64 | 64 | 0.0730 |
| UNC | #2-56 | 56 | 0.0860 |
| UNC | #3-48 | 48 | 0.0990 |
| UNC | #4-40 | 40 | 0.1120 |
| UNC | #5-40 | 40 | 0.1250 |
| UNC | #6-32 | 32 | 0.1380 |
| UNC | #8-32 | 32 | 0.1640 |
| UNC | #10-24 | 24 | 0.1900 |
| UNC | #12-24 | 24 | 0.2160 |
| UNC | 1/4-20 | 20 | 0.2500 |
| UNC | 5/16-18 | 18 | 0.3125 |
| UNC | 3/8-16 | 16 | 0.3750 |
| UNC | 7/16-14 | 14 | 0.4375 |
| UNC | 1/2-13 | 13 | 0.5000 |
| UNC | 9/16-12 | 12 | 0.5625 |
| UNC | 5/8-11 | 11 | 0.6250 |
| UNC | 3/4-10 | 10 | 0.7500 |
| UNC | 7/8-9 | 9 | 0.8750 |
| UNC | 1-8 | 8 | 1.0000 |
| UNC | 1-1/8-7 | 7 | 1.1250 |
| UNC | 1-1/4-7 | 7 | 1.2500 |
| UNC | 1-1/2-6 | 6 | 1.5000 |
| UNF | #0-80 | 80 | 0.0600 |
| UNF | #2-64 | 64 | 0.0860 |
| UNF | #4-48 | 48 | 0.1120 |
| UNF | #6-40 | 40 | 0.1380 |
| UNF | #8-36 | 36 | 0.1640 |
| UNF | #10-32 | 32 | 0.1900 |
| UNF | #12-28 | 28 | 0.2160 |
| UNF | 1/4-28 | 28 | 0.2500 |
| UNF | 5/16-24 | 24 | 0.3125 |
| UNF | 3/8-24 | 24 | 0.3750 |
| UNF | 7/16-20 | 20 | 0.4375 |
| UNF | 1/2-20 | 20 | 0.5000 |
| UNF | 9/16-18 | 18 | 0.5625 |
| UNF | 5/8-18 | 18 | 0.6250 |
| UNF | 3/4-16 | 16 | 0.7500 |
| UNF | 7/8-14 | 14 | 0.8750 |
| UNF | 1-12 | 12 | 1.0000 |
| Metric coarse | M2 × 0.4 | 0.4 | 2.0 |
| Metric coarse | M2.5 × 0.45 | 0.45 | 2.5 |
| Metric coarse | M3 × 0.5 | 0.5 | 3.0 |
| Metric coarse | M4 × 0.7 | 0.7 | 4.0 |
| Metric coarse | M5 × 0.8 | 0.8 | 5.0 |
| Metric coarse | M6 × 1.0 | 1.0 | 6.0 |
| Metric coarse | M8 × 1.25 | 1.25 | 8.0 |
| Metric coarse | M10 × 1.5 | 1.5 | 10.0 |
| Metric coarse | M12 × 1.75 | 1.75 | 12.0 |
| Metric coarse | M14 × 2.0 | 2.0 | 14.0 |
| Metric coarse | M16 × 2.0 | 2.0 | 16.0 |
| Metric coarse | M20 × 2.5 | 2.5 | 20.0 |
| Metric coarse | M24 × 3.0 | 3.0 | 24.0 |
| Metric fine | M8 × 1.0 | 1.0 | 8.0 |
| Metric fine | M10 × 1.25 | 1.25 | 10.0 |
| Metric fine | M12 × 1.25 | 1.25 | 12.0 |
| Metric fine | M16 × 1.5 | 1.5 | 16.0 |
| Metric fine | M20 × 1.5 | 1.5 | 20.0 |
Fastener strengths are the specification minimum tensile strengths; tapped-material strengths are the typical values stated in this library's material guides, so the calculator agrees with the articles. Shear strength is taken as 0.6 × tensile throughout.[4]
| Bolt / external thread | Tensile strength (ksi) | Basis |
|---|---|---|
| SAE Grade 2 steel | 74 | SAE J429, sizes to 3/4 in |
| SAE Grade 5 steel | 120 | SAE J429, sizes to 1 in |
| SAE Grade 8 steel | 150 | SAE J429 |
| Alloy steel socket head cap screw | 170 | ASTM A574, sizes over 1/2 in (180 ksi up to 1/2 in) |
| 18-8 / 304 stainless fastener | 100 | ASTM F593 condition CW, sizes to 5/8 in |
| Ti-6Al-4V fastener | 130 | Typical, see the titanium guide |
| Tapped / internal material | Tensile strength (ksi) | From |
|---|---|---|
| 6061-T6 aluminum | 45 | 6061 vs 7075 vs 2024 |
| 7075-T7351 aluminum | 73 | 6061 vs 7075 vs 2024 |
| 2024-T351 aluminum | 70 | 6061 vs 7075 vs 2024 |
| A36 steel | 58 | A36 vs 1018 |
| 1018 cold drawn steel | 64 | A36 vs 1018 |
| 1045 steel | 91 | 1018 vs 1045 |
| 4140 pre-hard (28–32 HRC) | 130 | 4140 vs 4340 vs 4130 |
| 303 stainless | 90 | Stainless grades |
| 304 stainless | 84 | Stainless grades |
| 316 stainless | 84 | Stainless grades |
| 17-4 PH H900 | 190 | Stainless grades |
| Ti-6Al-4V | 130 | Titanium grades |
| CP titanium Grade 2 | 50 | Titanium grades |
| Delrin (acetal) | 10 | UHMW vs Delrin |
| UHMW polyethylene | 5.8 | UHMW vs Delrin |
C&W taps to the percent of thread the material wants, checks every tapped hole with go/no-go gages, and will flag a drawing whose thread depth cannot carry the fastener.