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CELE Steel & Timber DesignSteel Tension MembersCheat Sheet

A printable cheat sheet for Steel Tension Members, built for CELE reviewers who want one go-to reference in the final stretch. Covers formulas, key definitions, common question types, and the Professional Regulation Commission (PRC) — Board of Civil Engineering-specific twists you will see on CELE day.

Exam context

On the CELE 2026, the Steel & Timber Design subtest carries a "Core" weight in Professional Regulation Commission (PRC) — Board of Civil Engineering's pattern. Steel Tension Members lands at position 1st out of 5 in the standard review order. Target score is 70% weighted average, no sub-test below 50%, and roughly a meaningful share of items come from Steel & Timber Design on a typical CELE paper.

Steel Tension Members - Cheat Sheet

Your 30-minute exam survival guide for tension member design. Covers the two limit states, net-area calculation (staggered holes), shear lag, and block shear. Every formula, definition, and pitfall you need for the PRC licensure exam.

Sections

Formulas

Formula

φₜ Pₙ = 0.90 Fᵧ Aₘ (yielding)

Meaning

φₜ = 0.90 resistance factor; Fᵧ = specified yield strength (MPa); Aₘ = gross cross-sectional area (mm²); Pₙ = nominal strength

Watch Out

DO NOT use net area here — use the full gross area Ag. This represents plastic deformation over the entire member.

When To Use

Ductile failure — applies to the full, unpierced section; typically governs when Fy·Ag is low or holes are small.

Formula

φₜ Pₙ = 0.75 Fᵤ Aₑ (rupture)

Meaning

φₜ = 0.75 resistance factor (lower!); Fᵤ = ultimate (tensile) strength (MPa); Aₑ = effective net area (mm²); accounts for sudden brittle failure at holes.

Watch Out

The φ factor is 0.75 here (not 0.90) because rupture is sudden. Must use Aₑ, not Ag. Many students flip these φ values.

When To Use

Sudden, brittle fracture through the weakest cross-section (at bolt holes). Always calculate both and take the LOWER result.

Common Values

Value

0.90

Symbol

φₜ (tension yield)

Quantity

Resistance factor (yield)

Value

0.75

Symbol

φₜ (tension rupture)

Quantity

Resistance factor (rupture)

Value

1.67

Symbol

Ωₜ

Quantity

Safety factor — yield (ASD)

Value

2.00

Symbol

Ωₜ

Quantity

Safety factor — rupture (ASD)

Section Title

Two Limit States for Tension Design

Important Facts

  • Design strength = 0.90 Fy Ag (yield) or 0.75 Fu Ae (rupture) — CHOOSE THE LOWER ONE.
  • Yielding uses φ = 0.90 (higher) on Fy (lower); rupture uses φ = 0.75 (lower) on Fu (higher). This balance is why both must be checked.
  • LRFD required capacity: φ Pₙ ≥ Pu (factored load). ASD required capacity: Pₙ / Ω ≥ P (service load); Ωt = 1.67 (yield), 2.00 (rupture).
  • Ductility: yielding is gradual (allows redistribution); rupture is sudden (brittle). The lower φ for rupture reflects this severity.
  • If Fy Ag > Fu Ae, then rupture controls (lower design strength). If Fu Ae > Fy Ag, then yield controls.

Key Definitions

Term

Gross Area (Aₘ)

Example

A 200 × 12 mm plate has Aₘ = 200 × 12 = 2400 mm²

Definition

Full cross-sectional area of the member before subtracting holes.

Term

Net Area (Aₙ)

Example

Aₘ = 2400 mm²; two 22 mm holes → Aₙ = 2400 − 2(22)(12) = 1872 mm²

Definition

Gross area minus the area of all bolt holes along the failure path.

Term

Effective Net Area (Aₑ)

Example

For an angle bolted through one leg, U ≈ 0.85; if Aₙ = 1200 mm², then Aₑ = 0.85 × 1200 = 1020 mm²

Definition

Net area multiplied by shear-lag factor U to account for non-uniform stress transfer when only part of the section is connected.

Term

Shear-Lag Factor (U)

Example

Plate bolted through full width: U = 1.0; L-shape bolted one leg: U ≈ 0.85

Definition

Reduction factor (0 < U ≤ 1.0) accounting for stress concentration near the bolted connection; U = 1.0 only when all elements are connected.

Term

Hole Diameter (dₕ)

Example

20 mm bolt → dₕ = 22 mm (use 22 mm in net-area calculations, NOT 20 mm)

Definition

Nominal bolt diameter plus clearance allowance; typically dₕ = dᵦ + 2 mm (or + 3 mm per Philippine practice).

Diagrams To Know

  • Stress-strain diagram: flat yield plateau (ductile region) then upturn to failure (brittle rupture region).
  • Net section diagram: show all holes on one 'slice' of the member and shade the pierced area being subtracted.

Formulas

Formula

Aₙ = Aₘ − Σ(dₕ · t)

Meaning

Aₙ = net area; dₕ = hole diameter (bolt size + 2–3 mm allowance); t = material thickness; Σ = sum for all holes in the failure path.

Watch Out

Use dₕ (full hole size with clearance), NOT the bolt diameter. Example: 20 mm bolt has dₕ = 22 mm. Subtract this for each hole.

When To Use

Straight-line hole arrangement (all holes in one transverse line perpendicular to member axis).

Formula

Net width = Wₘ − Σ dₕ + Σ(s²/4g)

Meaning

Wₘ = gross width; dₕ = hole diameter; s = longitudinal pitch (spacing along member axis); g = transverse gage (perpendicular spacing); s²/4g term added once per staggered diagonal segment.

Watch Out

The s²/4g term ADDS back (reduces the subtraction). It represents the 'benefit' of stagger. Easy to forget or apply incorrectly. Check every possible zig-zag path.

When To Use

Staggered bolt holes. Multiple failure paths exist; the minimum net area governs. Calculate all possible paths and use the smallest.

Formula

Aₙ = (Net width) × t

Meaning

Net area equals the minimum net width multiplied by thickness.

Watch Out

Always check ALL possible failure paths through staggered holes — don't assume the straight path is minimum.

When To Use

After computing the minimum net width (especially with staggered holes), convert to area by multiplying by thickness.

Section Title

Net Area Calculation: Straight & Staggered Holes

Important Facts

  • For staggered holes, draw and check EVERY possible path (not just the obvious straight line). The minimum net area from all paths governs.
  • The s²/4g term is added only for diagonal segments; it partially restores width lost to holes in the zig-zag path.
  • Common practice: dₕ = dᵦ + 2 mm for Standard holes (Philippine codes often use +3 mm); clarify with local standards.
  • If multiple holes exist in one transverse line, subtract all of them in that line.
  • Stagger is beneficial: it allows load to bypass some holes, so net area improves vs. all holes in one line.

Key Definitions

Term

Pitch (s)

Example

Holes at 50 mm spacing along a truss member: s = 50 mm

Definition

Distance between consecutive hole centers measured along the member axis (longitudinal direction).

Term

Gage (g)

Example

Two bolt lines 75 mm apart: g = 75 mm

Definition

Distance between hole centers measured perpendicular to the member axis (transverse direction), between two lines of holes.

Term

Failure Path

Example

A staggered pattern may have paths that drop diagonally (zig-zag) to avoid some holes, reducing loss vs. a straight path.

Definition

The imaginary line connecting holes that represents the weakest cross-section through the member; can be straight or zig-zag (staggered).

Diagrams To Know

  • Plan view of staggered bolt pattern: show grid with hole positions, draw zig-zag failure paths, label s and g.
  • Cross-section showing net width reduction: shade the bolt-hole area subtracted and label the stagger 'recovery'.

Formulas

Formula

Aₑ = U · Aₙ

Meaning

Aₑ = effective net area used in rupture check; U = shear-lag reduction factor (0 < U ≤ 1.0); Aₙ = net area.

Watch Out

Do NOT use Aₑ in the yielding formula — use gross area Ag. Shear lag only affects rupture. Confusing these is a major exam mistake.

When To Use

Always, when computing rupture strength (0.75 Fu Aₑ). U accounts for non-uniform stress distribution in the connected element.

Common Values

Value

1.0

Symbol

U

Quantity

Shear-lag factor — plate (full width)

Value

0.85 (typical, per AISC)

Symbol

U

Quantity

Shear-lag factor — angle (one leg bolted)

Value

0.90 (typical, per AISC)

Symbol

U

Quantity

Shear-lag factor — tee (one flange bolted)

Section Title

Shear-Lag Factor (U) & Effective Net Area

Important Facts

  • U accounts for the fact that stress at the bolted edge is higher than at the free edge due to shear lag.
  • NSCP 2015 / AISC 360 provides U-value tables for standard shapes (angles, tees, channels). Typical: angles ≈ 0.85, tees bolted one flange ≈ 0.90.
  • For a plate bolted through the full width with holes going through both edges, U = 1.0 (no lag).
  • If the distance from the bolts to the far edge is large relative to the connected length, U decreases further.
  • Aₑ is ONLY used in the rupture formula (0.75 Fu Aₑ), never in the yield formula.

Key Definitions

Term

Shear Lag

Example

An L-section bolted through only one leg; the unbolted leg stretches slightly more (lower stress), reducing average stress.

Definition

Non-uniform stress distribution near a bolted connection where some cross-sectional elements (e.g., one leg of an angle) are connected, leaving other parts (e.g., the other leg) to lag behind in load transfer.

Term

U = 1.0 Condition

Example

Flat plate bolted through its full width (bolt holes span the entire width); U = 1.0

Definition

Full effective net area applies when the member geometry and connection transfer load uniformly to all elements (entire section is actively connected).

Term

U < 1.0 Condition

Example

Angle L75×75 bolted through the short leg only; U ≈ 0.85 (some typical values: U = 0.85 for angles, 0.90 for tees)

Definition

Reduction applies when only part of the cross-section is bolted (e.g., one leg of an angle or one flange of a tee).

Diagrams To Know

  • Shear-lag diagram: angle bolted through one leg, showing stress concentration at the bolted leg vs. lower stress at the free leg.
  • Comparison of U-values for different member types: plate (U=1.0), angle (U≈0.85), tee (U≈0.90).

Formulas

Formula

Rₙ = 0.60 Fᵤ Aₘᵥ + 0.50 Fᵧ Aₙₜ ≤ 0.60 Fᵤ Aₙᵥ + 0.50 Fᵧ Aₙₜ (LRFD)

Meaning

Rₙ = nominal block shear strength; Aₘᵥ = gross shear area; Aₙᵥ = net shear area; Aₙₜ = net tension area; Fᵤ = ultimate strength; Fᵧ = yield strength.

Watch Out

Block shear is often OMITTED in undergraduate courses but appears on the PRC exam. Always check it for bolted connections. Use the LOWER of the two terms.

When To Use

When bolt group or welded connection could fail by combined shear along one plane and tension across another (e.g., at the perimeter of a bolt group attached to a plate or gusset).

Common Values

Value

0.60 Fu

Symbol

block shear

Quantity

Shear rupture stress coefficient

Value

0.50 Fy

Symbol

block shear

Quantity

Tension rupture stress coefficient

Value

0.75

Symbol

φ

Quantity

Resistance factor — block shear

Section Title

Block Shear (Tension-Shear Rupture)

Important Facts

  • Block shear check is MANDATORY for connections (often forgotten by students).
  • Design strength for block shear = φ Rₙ, where φ = 0.75 (same as rupture).
  • The formula has two terms: shear rupture (0.60 Fu Aₙᵥ) and combined shear-tension. Use the LOWER result.
  • Common in bolted angles and tees where a corner 'block' of material can tear free.
  • Calculate using the lesser of: (1) all gross shear + net tension, or (2) net shear + net tension.

Key Definitions

Term

Block Shear

Example

Angle connection where bolt group tears along the edge (shear) and tears through the net section (tension); material 'blocks' out.

Definition

A combined failure mode where a block of material tears out due to shear along one direction and tension along a perpendicular direction simultaneously.

Term

Shear Area (Aᵥ)

Example

For an angle bolted at two bolt lines, Aᵥ = (number of bolt rows) × (edge distance) × (thickness)

Definition

Gross or net cross-sectional area along which shear rupture can occur (parallel to the applied load or connection edge).

Term

Tension Area (Aₜ)

Example

Net width across the bolt holes times thickness.

Definition

Net cross-sectional area perpendicular to the shear area where tension failure (rupture through holes) occurs.

Diagrams To Know

  • Block shear tear pattern: show a rectangular block of material tearing along two perpendicular faces (one shear, one tension).
  • Bolt pattern with block shear boundary highlighted: corner distance and edge spacing labeled.

Formulas

Formula

L/r ≤ 300 (recommended)

Meaning

L = member length; r = least radius of gyration; recommendation to limit vibration/sag in tension members.

Watch Out

This is a RECOMMENDATION, not a hard code requirement. However, exam questions may ask you to verify it. For rods, the check is often waived.

When To Use

Check after designing the member size. This is NOT a strength limit (tension members do not buckle) but a serviceability recommendation.

Common Values

Value

≤ 300

Symbol

L/r

Quantity

Recommended slenderness ratio limit

Value

≤ 400

Symbol

L/r

Quantity

Typical rod (relaxed limit)

Section Title

Slenderness & Practical Design

Important Facts

  • Tension members do NOT buckle (no compression); slenderness limits are for sag, vibration, and handling only.
  • L/r ≤ 300 is good practice; sometimes relaxed to 400 for rods in remote locations.
  • Radius of gyration r = √(I/A), where I = second moment of inertia, A = cross-sectional area.
  • Always use the SMALLEST r value (about the the weakest axis, usually the minor axis).
  • Verify L/r after you've determined the member size; if too large, increase the cross-section.

Key Definitions

Term

Slenderness Ratio (L/r)

Example

A rod 5 m long with r = 20 mm: L/r = 5000/20 = 250 (acceptable, < 300)

Definition

The ratio of member length to the least radius of gyration; a measure of how 'thin' or 'stretched' the member is.

Diagrams To Know

  • Sag and vibration diagram: show a long, thin member deflecting sideways under its own weight or dynamic loading.

Common Values

Value

+2 to +3 mm over bolt diameter

Symbol

dₕ

Quantity

Hole size allowance (standard)

Value

1.5 × dₕ

Symbol

edge distance

Quantity

Minimum edge distance (standard hole)

Value

3 × dᵦ (approximately)

Symbol

s

Quantity

Minimum pitch

Section Title

Connection & Bolt Details

Important Facts

  • All tension member connections must be checked for bolt shear, bearing, and block shear (in addition to member strength).
  • Staggered holes are beneficial: they increase net area vs. straight-line holes.
  • Welds (fused connections) do NOT have net area reduction, so Aₑ = Aₘ for welded tension members.
  • Use dₕ = dᵦ + 2 or 3 mm for punched/drilled holes; clarify the standard for your exam jurisdiction.
  • Edge distance must meet minimum code requirements (typically 1.5 × hole diameter for standard holes).

Key Definitions

Term

Standard Hole

Example

Ø20 bolt → standard hole diameter = 22 mm (not 20 mm)

Definition

Bolt hole with nominal diameter = bolt diameter + 2 mm (or +3 mm per local Philippine practice). Use for net-area calculations.

Term

Edge Distance

Example

Bolt 50 mm from the edge; edge distance = 50 mm

Definition

Distance from the center of a bolt hole to the nearest edge of the member, measured perpendicular to the edge.

Term

Minimum Pitch

Example

Ø20 bolts: minimum pitch ≈ 60 mm

Definition

Minimum spacing between bolt centers along the axis of the member; typically 3 × bolt diameter.

Diagrams To Know

  • Bolt hole layout: plan view showing pitch, gage, and edge distances; staggered pattern with failure paths.
  • Cross-section through bolted joint: show member thickness, hole diameter, and washer bearing area.

Must Remember

  • ALWAYS CHECK BOTH LIMIT STATES: φ Pₙ = 0.90 Fy Aₘ (yield) AND φ Pₙ = 0.75 Fu Aₑ (rupture). The LOWER value governs the design strength.
  • Use dₕ = dᵦ + 2 or 3 mm for net area calculations, NOT the bare bolt diameter. Subtract this full hole size from gross area.
  • For staggered holes, evaluate ALL possible zig-zag failure paths. The path with the MINIMUM net area governs; s²/4g term adds (recovers) width on diagonal segments.
  • Aₑ = U·Aₙ: apply the shear-lag factor U ONLY in the rupture formula (0.75 Fu Aₑ), NEVER in the yield formula. U = 1.0 for plates bolted full width; U < 1.0 for angles, tees (typical: 0.85, 0.90).
  • DO NOT forget block shear (combined shear + tension rupture). It is a common exam item and often the governing failure mode at connections. φ Rₙ = 0.75(shear + tension).
  • For LRFD design: φ Pₙ ≥ Pu (required). For ASD: Pₙ/Ω ≥ P. Use φ = 0.90, Ω = 1.67 (yield); φ = 0.75, Ω = 2.00 (rupture).
  • Tension members do NOT buckle, so there is no buckling limit state. L/r ≤ 300 is a RECOMMENDATION for sag/vibration, not a code requirement.
  • Shear-lag factor accounts for non-uniform stress when only part of the section is bolted. U < 1.0 reduces the effective net area, making rupture more likely.
  • For welds (fused connections), there is no net area reduction: Aₑ = Aₘ and U = 1.0 (no holes, full section transfers load uniformly).
  • Always verify that your final member size satisfies L/r ≤ 300 (serviceability) and passes both yield and rupture strength checks under factored loads.

Last Minute Tips

  • Rig your sketches: always draw the member with bolt holes marked, label dₕ, s, g, and show which limit state controls. A clear sketch catches mistakes (e.g., forgetting a hole, wrong failure path).
  • Plug φ-factor and area into BOTH formulas first, then compare: if 0.90(248)(2400) = 535.7 kN and 0.75(400)(1872) = 561.6 kN, the first (535.7 kN) governs, so take that one. Order matters: yield first, rupture second, then compare.
  • For staggered holes, the trick is the s²/4g term: draw a grid, mark every hole, then trace each zig-zag path from left to right. The path that avoids the most holes (or has the largest stagger) wins. Use the SMALLEST net width you find.
  • Block shear sneaks onto many exams: the formula is complex, but the concept is simple—material tears in an L-shaped pattern at the connection corner. If a question gives you bolt spacing and edge distance, block shear is coming.
  • Don't panic if U is not given explicitly: AISC 360 Appendix D has standard U-values by shape (angle = 0.85, etc.). In exam mode, if you see 'angle bolted one leg,' assume U = 0.85 unless told otherwise.

Comparison Tables

Rows

Values

  • Gradual plastic deformation (ductile)
  • Sudden brittle fracture (brittle)

Property

Failure Mode

Values

  • Gross area Aₘ (full section)
  • Effective net area Aₑ = U·Aₙ (at holes)

Property

Area Used

Values

  • Fy (yield strength, ~248–400 MPa)
  • Fu (ultimate strength, ~400–500 MPa)

Property

Stress Used

Values

  • 0.90 (higher, safer)
  • 0.75 (lower, reflects suddenness)

Property

Resistance Factor φ

Values

  • 1.67
  • 2.00

Property

Safety Factor Ω (ASD)

Values

  • 0.90 Fy Aₘ
  • 0.75 Fu Aₑ

Property

Design Strength

Values

  • The LOWER of the two results
  • The LOWER of the two results

Property

Which Governs?

Values

  • Few/small holes or low Fu/Fy ratio
  • Multiple large holes or high Fu/Fy ratio

Property

Typical When

Columns

  • Aspect
  • Tensile Yield
  • Tensile Rupture

Table Title

Yield vs. Rupture Limit States

Rows

Values

  • Full width bolted
  • 1.0
  • Entire section connected uniformly

Property

Flat Plate

Values

  • One leg bolted
  • 0.85
  • Other leg lags; AISC specifies 0.85 standard

Property

Angle

Values

  • One flange bolted
  • 0.90
  • Web lags slightly

Property

Tee

Values

  • Bolted web
  • 0.75–0.85
  • Both flanges lag; varies with connection pattern

Property

Channel

Values

  • Bolted flanges only
  • 0.75
  • Web is unconnected; significant lag

Property

I-Beam

Columns

  • Member Type
  • Connection Type
  • Typical U Value
  • Notes

Table Title

Shear-Lag Factor (U) Values by Member Type

Rows

Values

  • Use dₕ = dᵦ + 2 or 3 mm, not dᵦ
  • Net area too large → underestimated strength → structural unsafe → FAIL

Property

Using bolt diameter instead of hole diameter in net area

Values

  • Use gross area Aₘ for yield; Aₑ only for rupture
  • Yield strength overstated → safe, but inefficient design

Property

Using net area in yield formula

Values

  • Always apply U for rupture: Aₑ = U·Aₙ
  • Rupture strength overstated → UNSAFE

Property

Forgetting shear-lag factor U

Values

  • Yield: φ = 0.90; Rupture: φ = 0.75
  • Design strength wrong → either unsafe or overly conservative

Property

Flipping φ = 0.90 and 0.75

Values

  • Always include block shear check for bolted connections
  • Hidden failure mode → unsafe design → FAIL on exam

Property

Not checking block shear

Values

  • Draw and evaluate every possible staggered path; use minimum net area
  • Missed true failure path → overestimated strength → UNSAFE

Property

Not considering all zig-zag failure paths

Values

  • L/r ≤ 300 is a SERVICEABILITY (sag/vibration) recommendation, not strength
  • May incorrectly reject a valid design or vice versa

Property

Confusing L/r as a STRENGTH limit

Columns

  • Mistake
  • Correct Approach
  • Exam Consequence

Table Title

Common Mistakes & Corrections

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