3

Steel Material Properties and Shapes

01

Engineering story

A century of steel — from concept to skyline

Engineer reviewing blueprints against a steel-frame construction site at sunrise

You cannot design what you cannot specify.

Fy and Fu — plus the right shape family — control every AISC calculation.

Chapter 3 covers ASTM specifications, the stress–strain curve, and the shape families (W, HP, HSS, angle, channel) that populate the AISC Shapes Database.

Iconic steel structures built on engineering excellence
  1. A36 mild-steel standard
    1960
  2. A992 introduced for W-shapes
    1998
  3. A500 Gr. C HSS grade
    2013
  4. AISC 360-22 material provisions
    2022
Load pathMill certificationASTM specAISC Shapes DBSection propertiesDesign check
02

Learning objectives

What you will be able to do after finishing Chapter 1 — and why each objective matters in practice

Specify the right ASTM gradeObjective 01

Specify the right ASTM grade

A992 (Fy=50, Fu=65) is the standard for rolled W-shapes; A500 Gr. C for HSS; A36 for plates and angles.

Why it matters
Wrong grade = wrong Fy = wrong capacity.
Where it is used
Every AISC calc.
Connects to
AISC A3.1.
Read the stress–strain curveObjective 02

Read the stress–strain curve

E = 29,000 ksi elastic; yield plateau at Fy; strain-hardens to Fu; ruptures at ~15-25% strain.

Why it matters
Ductile steel warns before failure — brittle steel does not.
Where it is used
Plastic design, seismic detailing.
Connects to
Mechanics of materials; A3.
Navigate shape familiesObjective 03

Navigate shape families

W (flexure), HP (piles), HSS (columns/braces), L (tension), C/MC (secondary).

Why it matters
The right family halves the material weight.
Where it is used
Preliminary sizing.
Connects to
AISC Manual Part 1.
Look up section propertiesObjective 04

Look up section properties

For each shape: A, d, bf, tf, tw, Ix, Iy, Sx, Sy, Zx, Zy, rx, ry, J, Cw.

Why it matters
AISC formulas plug these directly.
Where it is used
Every strength and stiffness check.
Connects to
AISC Manual Part 1.
Fracture toughness and CVNObjective 05

Fracture toughness and CVN

Charpy V-Notch impact tests screen brittle behaviour at low temperature; AISC-Seismic requires demand-critical welds to satisfy CVN targets.

Why it matters
Brittle fracture is sudden and total.
Where it is used
Cold-region and seismic design.
Connects to
AISC Seismic A3.4.
Durability & corrosionObjective 06

Durability & corrosion

Painted, galvanised, or weathering steel (A588). Loss of section from corrosion reduces Ag and Fy relevance.

Why it matters
50-year service demands corrosion strategy from day 1.
Where it is used
Exposed structures, bridges.
Connects to
AISC/SSPC guidance.
03

Engineering motivation

What each part of a steel-frame building actually does — and why it exists

Before you design any single member, you have to see the whole system. A steel-frame building is not a collection of independent shapes bolted together — it is a deliberate load path, engineered so that every kilonewton of gravity, wind, or seismic demand has a continuous route from where it starts to the ground where the earth can resist it.

The photograph below shows a typical steel framing detail. Drag each labelled chip onto the structural element it names — the drop is only accepted when it lands inside the correct element's outlined region. A correct answer locks in with a green outline and a short explanation; a wrong answer flashes the region red, tells you what you actually hit, and returns the chip so you can try again. Press Reveal expected placements to see the reference solution (that attempt is then marked as assisted).

Structural steel framing — identify each element by dragging the labels
Fig. 1.3 · Drop a chip inside the outlined element it names. Green = correct and locked; red flash = wrong element, chip returns.
04

Failure mechanisms

Why we design the way we do — six ways steel structures have failed, and what each disaster taught the profession

Every provision in AISC 360 is a scar. Behind each equation, load factor, and detailing rule is a bridge, a walkway, or a tower whose failure cost lives and rewrote the profession. The six case studies below trace the mechanisms that motivate the code you are about to learn.

Read each one as an engineer, not a spectator: identify the load, the limit state, the missing check, and the specific clause that exists today because that check was missed. When you meet those clauses again in Chapters 5–17, they will read as answers, not rules.

Brittle fracture: Cold-temperature cleavage fracture with little plastic warning.
Case 01
Fig. 1.4.1 · Brittle fracture
Failure mechanism

Brittle fracture

Cold-temperature cleavage fracture with little plastic warning.

Root cause

Low toughness, notch, tri-axial restraint.

Lesson learned
Specify CVN toughness for demand-critical welds; avoid sharp re-entrant corners.
§AISC 360-22 A3.1c / AISC Seismic
Corrosion / section loss: Rust reduces effective Ag and creates local pits.
Case 02
Fig. 1.4.2 · Corrosion / section loss
Failure mechanism

Corrosion / section loss

Rust reduces effective Ag and creates local pits.

Root cause

Water + oxygen + no coating.

Lesson learned
Paint, galvanise, or use weathering steel; inspect on schedule.
§SSPC / AISC durability
How failure propagates
The five-stage failure progression
1Mill cert
2Elastic response
3Yield plateau
4Strain hardening
5Rupture

Design codes intervene at the transition from yield to instability. Everything before yield is elastic and reversible; everything after instability is a race to collapse. LRFD keeps the demand well below the first transition.

05

Lecture notes

The full textbook chapter — figures, equations, and engineering narrative

Reflection · Think before you read

Two beams have identical geometry but one is A36 and the other is A992. Before running any numbers, where do you expect their behavior to differ — yielding, deflection, ductility, weldability, cost?

Structural materials: families, properties, and choosing one

Structural design is the planned organization of materials and components to safely resist internal and external forces — dead, live, and environmental loads — without exceeding strength or serviceability limit states. Choosing the right material means balancing strength, stiffness, durability, weight, and economy for the specific load path, exposure, and budget in front of you.

Structural steel used in structural construction

Structural steel

AISC 360-22 / AISC 341
  • Ductile: yields visibly and redistributes force before fracture.
  • Members are prefabricated — dimensional control and shop QA are excellent.
  • Loses ~50% of yield strength near 1100 °F; needs spray-on or board fireproofing.
Reinforced concrete used in structural construction

Reinforced concrete

ACI 318-19
  • Monolithic construction gives inherent continuity and redundancy.
  • Design is under-reinforced on purpose so steel yields first (ductile warning).
  • Self-weight is often 60–70% of total gravity load in a concrete frame.
Timber / mass timber used in structural construction

Timber / mass timber

NDS / AWC
  • Renewable and carbon-storing — strongest sustainability case of the six.
  • Engineered products (Glulam, LVL, CLT) remove knots and raise reliability.
  • Anisotropic: never rely on tension perpendicular to grain.
UHPC used in structural construction

UHPC

ACI 239 / AASHTO UHPC guidance
  • Fiber bridging lets it carry tension after cracking — unusual for a cementitious material.
  • Often eliminates conventional shear reinforcement in thin members.
  • Life-cycle cost, not first cost, is the argument for UHPC.
Masonry used in structural construction

Masonry

TMS 402/602
  • Unreinforced masonry is prohibited in high seismic design categories.
  • Grouted cells with vertical bars convert brittle walls into ductile shear walls.
  • Control joints are mandatory to manage shrinkage and thermal movement.
FRP composites used in structural construction

FRP composites

ACI 440.2R / 440.11
  • No ductility: the structure must retain ductility from the substrate, not the FRP.
  • Typical use is upgrading an existing member, not designing a new primary frame.
  • Resin glass-transition temperature limits fire performance.
Table 3-A · Comparison of structural material families
PropertyStructural steelReinforced concreteTimber / mass timberUHPCMasonryFRP composites
StrengthFy = 50 ksi (A992); equal in tension & compressionf'c = 4–8 ksi compression; tension carried by rebar (fy = 60 ksi)Fb ≈ 0.9–3 ksi parallel to grain; weak perpendicular to grainf'c = 18–30 ksi; sustained post-crack tension from steel fibersf'm = 1.5–3 ksi compression; essentially no reliable tensionTensile 100–400 ksi (CFRP); linear elastic to rupture — no yielding
StiffnessE = 29,000 ksiEc ≈ 57,000√f'c psi; mass helps dampingE ≈ 1,300–2,000 ksiEc ≈ 7,000–8,500 ksiEm ≈ 900 f'm; stiff but brittleE = 6,000 ksi (GFRP) to 20,000+ ksi (CFRP)
Weight490 pcf, but very high strength-to-weight150 pcf — heavy self-weight drives foundations25–40 pcf — lightest structural option155 pcf, but sections are far thinnerHeavy — 100–140 pcf walls≈ 1/5 of steel — installs without cranes
DurabilityCorrodes — paint, galvanize, or weathering steelExcellent fire and water resistance; cover controls corrosionDecay, moisture, and termites unless treated or kept dryNear-zero permeability — outstanding freeze-thaw and chloride resistanceExcellent weathering, thermal mass, and fire ratingImmune to corrosion; UV and elevated-temperature limits apply
EconomyHigh material cost, fast erection, low labor hoursLow material cost, high formwork/labor and cure timeLow cost in residential/light commercial; premium for glulam/CLTVery high per cubic yard; justified by thin sections and long lifeLow material cost, labor-intensive, local mason skill dependentHigh unit cost, very low installation and downtime cost
Best forLong spans, high tension, moment frames, retrofits, fast schedulesHeavy static loads, compression members, shear walls, slabs, parking, foundationsLight framing, short-to-medium spans, low-carbon mass-timber buildingsBridge field joints, thin architectural panels, overlays, blast/impact zonesBearing walls, shear walls in low/mid-rise, fire separations, façadesStrengthening/retrofit wraps, corrosive environments, non-magnetic structures, GFRP rebar
Watch out forFire protection required; stability (LTB, local buckling) governs oftenCracking/deflection serviceability; heavy seismic mass; long cure scheduleMoisture content, shrinkage, connection crushing, char rate in fireSpecialty mixing/curing; limited local supply; few prescriptive code provisionsBrittle in seismic shear unless reinforced and grouted; out-of-plane loadingBrittle failure — design with large strength-reduction factors; bond/debonding controls
Governing codeAISC 360-22 / AISC 341ACI 318-19NDS / AWCACI 239 / AASHTO UHPC guidanceTMS 402/602ACI 440.2R / 440.11

How engineers actually make the choice

Load path & stress type

Trace the force to the foundation first. Tension and long spans favor steel or FRP; sustained compression and bearing favor concrete or masonry; light gravity framing favors timber.

Stiffness & serviceability

Strength rarely governs slender systems — deflection, drift, and floor vibration do. Compare EI and mass before choosing, not after sizing.

Environmental exposure

Assess humidity, freeze-thaw cycling, de-icing salts, and industrial chemicals. Corrosive exposure pushes toward concrete cover, galvanizing, UHPC, or FRP reinforcement.

Fire and life safety

Concrete and masonry are inherently rated; steel needs applied protection; timber relies on sacrificial char depth; FRP resins soften early.

Budget & constructability

Balance first cost against maintenance, formwork, crane access, schedule, and the skill available in the local labor market.

Sustainability

Compare embodied carbon, recycled content, recyclability, and renewable sourcing. Steel is highly recycled; timber sequesters carbon; cement clinker dominates concrete emissions.

Rule of thumb

Steel for long spans and tension. Concrete for heavy static compression, fire, and water. Timber for light, low-carbon framing. Masonry for bearing and shear walls with thermal mass. UHPC for thin, aggressive-exposure elements. FRP for corrosion-driven retrofits — never as the sole source of ductility.

Worked Example 3.1 — Material Properties from a Tension Coupon Test

Given: An ASTM A992 tension coupon has a gauge length Lo = 8.00 in and cross-sectional area Ao = 0.500 in². Selected data from the pull test:
  • At P = 12.0 k the elongation ΔL = 0.00662 in (still elastic).
  • Upper yield load Py = 25.5 k.
  • Ultimate load Pu,max = 32.8 k at ΔL = 0.72 in.
  • After unloading from a point at ΔL = 0.048 in, permanent set = 0.040 in.
  • A parallel 0.2% offset line intersects the curve at σ = 51.2 ksi.
Engineering stress–strain curve (mild structural steel) ε σ 0.2% offset yield εy Fy Fu Elastic (slope = E) yield plateau strain hardening necking
Engineering stress–strain response

Step 1 — Modulus of elasticity, E

Formula
(1)
σ = 12.0 / 0.500 = 24.0 ksi
ε = 0.00662 / 8.00 = 8.275 × 10⁻⁴
E = 24.0 / 8.275×10⁻⁴ = 29,000 ksi (matches AISC nominal value)

Step 2 — Yield strength Fy (upper yield point)

Formula
(2)
Fy = 25.5 / 0.500 = 51 ksi (satisfies A992: Fy ≥ 50 ksi)

Step 3 — 0.2% offset yield strength

Definition
(3)
its intersection with the curve is F_{y,0.2%}.
From the plot, Fy,0.2% = 51.2 ksi. This method governs for steels without a sharp plateau (e.g. high-strength or cold-worked bars).

Step 4 — Ultimate (tensile) strength Fu

Formula
(4)
Fu = 32.8 / 0.500 = 65.6 ksi (A992 requires 65 ≤ Fu ≤ 80 ksi ✓)

Step 5 — Plastic strain from an unload cycle

Formula
(5)
εtotal = 0.048/8.00 = 6.00 × 10⁻³
εplastic = 0.040/8.00 = 5.00 × 10⁻³
εelastic = 1.00 × 10⁻³ (recovered on unloading; check: σ/E = 29·10⁻³ / 29 ≈ 1.0×10⁻³ ✓)

Step 6 — Ductility check

Formula
(6)
% elongation = 0.72/8.00 × 100 = 9.0% in 8 in (A992 requires ≥ 18% in 8 in — actual coupons routinely exceed 20%; this reduced value is illustrative).
Coupon summary: E = 29,000 ksi · Fy = 51 ksi · Fu = 65.6 ksi · Fu/Fy = 1.29 (< 1.30 lower bound? A992 ≥ 1.10). Material is acceptable A992 steel.

Worked Example 3.2 — Section Properties of a Built-Up I-Shape

Given: A doubly-symmetric welded I-shape:
  • Flanges: 8 in × 0.5 in (top & bottom)
  • Web: 11 in × 0.375 in (clear between flanges)
  • Overall depth d = 12.0 in
  • Steel: A992 (Fy = 50 ksi)
Compute A, ȳ (centroid), Ix, Sx, Zx, and the shape factor.
Built-up I-shape — centroid & section moduli x (N.A.) bf = 8″ d = 12″ tf=½″ tw=⅜″
Cross-section geometry & neutral axis

Step 1 — Areas of the three plate elements

Formula
(7)
Atf = 8 × 0.5 = 4.00 in²
Aw = 11 × 0.375 = 4.125 in²
Abf = 8 × 0.5 = 4.00 in²
A = 12.125 in²

Step 2 — Centroid ȳ (measure from bottom of section)

Formula
(8)
ȳbf = 0.25 in, ȳw = 0.5 + 11/2 = 6.00 in, ȳtf = 11.75 in
Σ(Aȳ) = 4.00(0.25) + 4.125(6.00) + 4.00(11.75) = 1.00 + 24.75 + 47.00 = 72.75 in³
ȳ = 72.75 / 12.125 = 6.00 in — coincides with mid-depth (doubly symmetric ✓)

Step 3 — Moment of inertia Ix (parallel-axis theorem)

Formula
(9)
Top flange: Io = 8(0.5)³/12 = 0.0833; d = 6.00 − 0.25 (below top) → 6.00 − 11.75 = 5.75 → d = 5.75 in; A·d² = 4.00(5.75)² = 132.25
Web: Io = 0.375(11)³/12 = 41.59; d = 0 (centered on N.A.); A·d² = 0
Bottom flange: Io = 0.0833; d = 5.75 in; A·d² = 132.25
Ix = 2(0.0833 + 132.25) + 41.59 = 306.3 in⁴

Step 4 — Elastic section modulus Sx

Formula
(10)
c = 12.0/2 = 6.00 in; Sx = 306.3 / 6.00 = 51.05 in³

Step 5 — Plastic section modulus Zx

Formula
(11)
Distances of plate centroids from the PNA (mid-depth):
Flanges: |ȳ| = 6.00 − 0.25 = 5.75 in; contribution = 2 · 4.00 · 5.75 = 46.00 in³
Web (treat as two 5.5-in halves about the PNA): each half A = 5.5·0.375 = 2.0625 in², centroid 2.75 in from PNA; contribution = 2 · 2.0625 · 2.75 = 11.34 in³
Zx = 46.00 + 11.34 = 57.34 in³

Step 6 — Shape factor and design moments

Formulas
(12)
Shape factor = 57.34 / 51.05 = 1.12 (typical for W-shapes ≈ 1.10–1.15)
My = 50 · 51.05 = 2,553 k·in = 212.7 k·ft (first-yield moment)
Mp = 50 · 57.34 = 2,867 k·in = 238.9 k·ft (fully-plastic moment)
φb Mn = 0.90 · Mp = 215.0 k·ft (compact, fully braced)
Built-up I: A = 12.13 in² · Ix = 306.3 in⁴ · Sx = 51.05 in³ · Zx = 57.34 in³ · shape factor 1.12 · Mp = 238.9 k·ft.

Step 7 — Why do Sx, Zx, and the shape factor matter?

Design relevance of each quantity:
  • Elastic section modulus Sx pins down the first-yield moment My = Fy·Sx. Below My the whole section is elastic and the σ = M·c/I formula applies — Sx is what you use in serviceability (deflection, fatigue, elastic bending stress) checks.
  • Plastic section modulus Zx gives the fully-plastic moment Mp = Fy·Zx, the strength AISC 360-22 §F2 uses for the LRFD design moment φbMn of a compact, laterally-braced beam. Zx — not Sx — is the number tabulated in Manual Table 3-2 and the value you compare demand to when sizing a beam.
  • Shape factor f = Zx/Sx measures the reserve strength between first yield and full plastification: (Mp − My)/My = f − 1. For this built-up I, f = 1.12 → 12% reserve above first yield. Values ≈ 1.10–1.15 for W-shapes, 1.5 for rectangles, 1.7 for solid rounds; the higher the shape factor, the more inefficient the section is at putting material near the extreme fibre.
  • Why LRFD design uses Mp, not My. A compact section can develop the plastic moment before local buckling; stopping the strength check at My would waste roughly (f − 1)·100 % of the section's capacity. That is why AISC anchors the flexural design equation on Zx.
  • Sanity check. If your computed f falls outside 1.10–1.20 for a W-shape or built-up I, something in the Sx/Zx calculation is wrong — usually a c = d/2 slip in Sx or a missed web-half in Zx.
Common pitfalls:
  • Confusing 0.2% offset yield (a construction on the σ–ε plot) with the upper/lower yield point. Only steels without a sharp plateau require the offset method.
  • Using the web clear height (11 in) instead of the full depth (12 in) when computing c = d/2 for Sx.
  • Forgetting that for a doubly-symmetric section the PNA and elastic N.A. coincide — for singly-symmetric sections you must locate the PNA by equal-area split before computing Z.
  • Reporting Sx and Zx without checking that the shape factor lands in the expected 1.10–1.20 range for I-shapes (sanity check).
06

Professional practice, safety & ethics

Material specification practice

Professional practice
  • Specify by ASTM designation and grade (A992 for W-shapes, A500 Gr. C for HSS, A572 Gr. 50 for plate) — never by 'Fy = 50 ksi' alone.
  • Require Mill Test Reports (MTRs) for all primary members and verify heat numbers against the shipment.
  • Check availability before specifying an exotic grade; substitution requests delay fabrication.
Safety in design & construction
  • Notch toughness (CVN) matters for thick plate, cold service, and seismic applications — specify it where fracture is credible.
  • Galvanizing thick weldments can cause cracking; coordinate the coating and welding sequence.
  • Fire protection is a material issue: unprotected steel loses ~50% of Fy near 1100 °F.
Engineering ethics
  • Unapproved material substitution to save cost, without EOR review, is a serious violation.
  • Never accept material without traceable documentation — counterfeit MTRs have appeared in the supply chain.
  • Report suspect material to the client and building official (NSPE II.1.a).
Ironworkers bolting a steel beam connection while tied off at height
Erection safety: OSHA Subpart R fall protection and stable temporary bracing.
Engineers reviewing sealed structural drawings across a conference table
Peer review and the engineer's seal: responsible charge and standard of care.

ABET / licensure link. These points map to ABET Student Outcomes 2 and 4 — engineering design within realistic constraints, and recognition of ethical and professional responsibilities. Expect NCEES FE and PE exam questions on the NSPE Code of Ethics, OSHA construction requirements, and the engineer's standard of care.

07

Cost analysis

Grade and shape selection economics

Approach
  • Higher-strength steel (A992 Gr. 50 vs A36) costs only a few percent more per pound but can cut 20–30% of the weight in strength-governed members.
  • Strength grades do not help stiffness-governed members — E is the same for all steels.
  • Availability drives price: use common shapes and grades; exotic sections carry mill minimums and lead time.
Worked cost example — A36 vs A992 for a strength-governed tension member
Basis: Same required φPn = 300 kip
Line itemQtyRateCost
A36 section, Ag = 9.3 in² (31.6 lb/ft, 30 ft)
0.47 ton @ A36$1,080$508
A992 section, Ag = 6.7 in² (22.5 lb/ft, 30 ft)
0.34 ton @ A992$1,150$391
Fabrication saved (lighter piece)
-0.13 ton$900−$117
Estimated total$782

Takeaway. The 50 ksi option is lighter and cheaper installed even at a higher $/ton — always price the installed member, not the coupon.

Unit rates are representative US averages for teaching purposes. On a real project, price with current local rates (RSMeans, fabricator quotes, or contractor pricing) and state the estimate date.

08

Animated concepts

Key mechanics visualised — watch the strain profile, stress block, or buckled shape evolve

Steel stress–strain curve
Fy=36Fu=58Stress-strain (A36 steel)Elastic (E = 29 000 ksi)

Elastic → yield plateau → strain hardening → necking. Fy sets design capacity; Fu sets rupture.

09

Engineering figures

Full-page reference diagrams — the visual vocabulary you will use for the rest of the course

§3.6.1

Shape yard

W, HSS, L, C stacked
Fig. 3.1W, HSS, L, C stacked

Match the family to the loading.

§3.6.2

Tensile test

Coupon in UTM
Fig. 3.2Coupon in UTM

Yield → strain-hardening → rupture.

§3.6.3

Brittle fracture

Cleavage surface
Fig. 3.3Cleavage surface

Little plastic warning.

§3.6.4

Corrosion

Section-loss beam
Fig. 3.4Section-loss beam

Coating is a design decision.

10

Worked examples

Full textbook solutions — problem, theory, step-by-step, verification, interpretation

Example 3.1

W14x90 (A992) — properties and shape factor

Lookup Fy, Fu, Sx, Zx from the AISC Manual and compute the shape factor.

Problem statement

Confirm ASTM properties and section properties for a W14x90 (A992), then compute its shape factor Zx/Sx.

Steel shape yard
FIG. 3.1 — the AISC Shapes Database is your first stop.
bfdtwtf
DIMW-shape geometry — d, bf, tf, tw drive every section property.
Given
  • W14x90 (A992)
  • AISC Manual Part 1
Find
  • Fy, Fu, Sx, Zx, Zx/Sx
Assumptions
  • Rolled, mill-certified shape
  • Room-temperature
Code references
  • ASTM A992
  • AISC Manual Part 1
Theory & approach

The shape factor bounds the plastic reserve above elastic Sx. For rolled W-shapes it is typically 1.10–1.15.

Step-by-step solution
  1. 1

    ASTM lookup

    FormulaASTM A992
    Fy = 50 ksi, Fu = 65 ksi
  2. 2

    AISC Manual Part 1

    W14x90: Ag = 26.5 in², Sx = 143 in³, Zx = 157 in³, rx = 6.14 in, ry = 3.70 in
  3. 3

    Shape factor

    Formula
    SF = Zx / Sx
    SF = 157 / 143 = 1.10
Final answer
Fy=50, Fu=65 ksi; Sx=143, Zx=157 in³; SF=1.10.
Common mistakes
  • Using A36 Fy=36 for a W-shape.
  • Confusing Sx (elastic) with Zx (plastic).
References
  • · ASTM A992
  • · AISC Manual 16th ed. Part 1
11

Guided practice

Compute the governing variables — hints unlock as you need them

Identify the specified minimum yield stress F_y and tensile stress F_u for (a) an A500 Grade C round HSS and (b) an A992 W-shape. State the modulus of elasticity E and comment on whether E differs between grades.

Your turn
Hints
  1. 1.Look up A500 Gr. C round HSS in AISC Manual Table 2-4: F_y = 46 ksi, F_u = 62 ksi.
12

Independent practice

Solve the chapter's design task — compute each governing variable

Design task

For A992 structural steel (Fy = 50 ksi, Fu = 65 ksi, E = 29,000 ksi), compute the yield strain εy, the strain-hardening strain εsh ≈ 10·εy, and the flange local-buckling slenderness limit λr = 0.56·√(E/Fy) for a rolled I-shape flange.

Given
  • Fy = 50 ksi
  • E = 29,000 ksi
  • εsh ≈ 10·εy (typical for mild steel)
Approach
  1. εy = Fy / E — the elastic strain at first yield.
  2. For A992, εsh is not a code number; use 10·εy as the lecture approximation.
  3. AISC Table B4.1b flange λr for rolled I-shapes: 0.56·√(E/Fy).
Submit your answer
13

Mini design challenge

Pick the shape family + ASTM grade that fits each application

Brief

Match the correct steel product/family AND specification to each application: 24-ft office floor beam, 12-ft interior gravity column, bolted single-angle brace diagonal, and a channel stair stringer. Cite AISC Manual Part 1 shape tables and Part 2 material tables.

Requirements
  • State the shape family (W, HSS, L, C)
  • State the preferred ASTM specification (Manual Table 2-4)
  • Explain WHY the shape/grade fits the load pattern
  • Note whether the grade is stocked / economical
14

Chapter summary

A mind map of how every concept connects

Fy, Fu, E, εuA992 (W-shape)A500 Gr. C (HSS)Shape familiesSection properties
Steel Material & Shapes (AISC 360-22 A3, Manual Part 1)

Graded Chapter Quiz(17 FE-style questions · AISC Manual required)

These questions reference AISC Steel Construction Manual (16th ed.) — sections, equations, and tables are cited explicitly. Use a calculator. Each question offers a clue you may reveal before answering. Submissions are recorded to your account once signed in.

C3-01AISC 360-22 §B4
1. Modulus of elasticity of structural steel (AISC 360-22 §B4) is:
C3-02AISC 360-22 §B4
2. Shear modulus G of steel:
C3-03ASTM A370
3. The 0.2% offset yield stress for a stress-strain curve reaching σ = 55 ksi at ε=0.005 (with slope 29,000 ksi through origin) is estimated by:
σ–ε curve · structural steel ε σ 0.2% offset Fy Fu εy yield plateau strain hardening necking
C3-04AISC Manual Table 2-4
4. For a W14×90 (A992), what is Fy per AISC Manual Table 2-4?
C3-05Mechanics of materials
5. Which is the 'plastic' modulus of a rectangular section b×h?
Rectangle b × h = 4″ × 8″ N.A. b = 4″ h = 8″ b h²/4 vs b h²/6
C3-06Mechanics
6. Centroid of a T-section (flange 6×1 in + stem 1×5 in, total depth 6 in from top of flange) measured from top:
T-section — find ȳ from top 1″ 5″ flange 6″ stem 1″
C3-07Mechanics
7. For a rectangular 4×8 in section (b=4, h=8, weak axis: b), Ix (in⁴):
Rectangle b × h = 4″ × 8″ N.A. b = 4″ h = 8″
C3-08Mechanics
8. Elastic section modulus Sx for the section in C3-07:
Rectangle b × h = 4″ × 8″ N.A. b = 4″ h = 8″
C3-09Mechanics
9. Plastic section modulus Zx for the section in C3-07:
Rectangle b × h = 4″ × 8″ N.A. b = 4″ h = 8″
C3-10AISC Manual Part 1
10. Which shape offers the best flexural efficiency (highest Z/A) among these?
C3-11ASTM A36
11. A hot-rolled A36 flat has Fy=36 ksi, Fu=58 ksi. Minimum required elongation in 8-in gauge per ASTM A36:
C3-12AISC 360-22 §B4
12. Coefficient of thermal expansion α for steel used for expansion joints:
C3-13AISC Manual Table 1-1
13. For a W16×36, from AISC Manual Table 1-1: Ix ≈ 448 in⁴, Sx ≈ 56.5 in³, Zx ≈ 64.0 in³. Shape factor Zx/Sx =?
C3-14AISC 360-22 §B4 / Mechanics of Materials
14. Structural steel has E = 29,000 ksi and Poisson's ratio ν = 0.30. Compute the shear modulus G.
C3-15Mechanics of Materials
15. A stainless-steel alloy has E = 28,000 ksi and G = 10,769 ksi. Back-calculate Poisson's ratio ν.
C3-16Mechanics of Materials
16. A high-strength alloy reports E = 30,000 ksi and ν = 0.28. What is G?
C3-17Mechanics of Materials
17. A shaft twists under pure torsion with shear strain γ = 0.0012 rad when the shear stress is τ = 13.4 ksi. If ν = 0.30, estimate the axial modulus E of the material.

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Q1 — An ASTM A36 structural steel plate is tested in tension. As force increases, the steel reaches a critical stress where it begins to permanently stretch and deform without any additional load. Which mechanical property marks this transition from elastic to plastic behavior?

◆ EasyASTM A36 · AISC 360-22 §A3