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CELE Engineering MechanicsCentroids and Moments of InertiaCheat Sheet

Cheat sheet for CELE Engineering Mechanics — Centroids and Moments of Inertia. Compact, printable, and organised around the concepts Professional Regulation Commission (PRC) — Board of Civil Engineering tests most frequently in the CELE 2026. Perfect for the week before exam day.

Exam context

On the CELE 2026, the Engineering Mechanics subtest carries a "Core" weight in Professional Regulation Commission (PRC) — Board of Civil Engineering's pattern. Centroids and Moments of Inertia lands at position 6th out of 8 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 Engineering Mechanics on a typical CELE paper.

Centroids and Moments of Inertia - Cheat Sheet

Your last-minute revision companion for Engineering Mechanics: centroids, moments of inertia, parallel-axis theorem, and radius of gyration. Every formula, definition, and board-exam pitfall condensed into one sheet.

Sections

Formulas

Formula

x̄ = (ΣAᵢxᵢ) / ΣAᵢ; ȳ = (ΣAᵢyᵢ) / ΣAᵢ

Meaning

x̄, ȳ = centroid coordinates; Aᵢ = area of part i; xᵢ, yᵢ = coordinates of part i centroid

Watch Out

HOLES ARE NEGATIVE AREAS — subtract both Ahole and its (xhole, yhole) contributions. Sign error here kills half the section.

When To Use

Always — to find geometric center of any composite (built-up) section

Formula

Rectangle: (x̄, ȳ) = (b/2, h/2) from corner

Meaning

b = width, h = height

Watch Out

This is from the corner/origin; if origin is elsewhere, recalculate.

When To Use

Rectangular parts in composite sections

Formula

Triangle: ȳ = h/3 from base; x̄ depends on orientation

Meaning

h = height measured perpendicular to base

Watch Out

h/3, NOT h/2. Common error: confusing with rectangle centroid at h/2.

When To Use

Triangular parts in composite L-, T-, or trapezoidal sections

Formula

Semicircle: distance from diameter = 4r/(3π)

Meaning

r = radius

Watch Out

Memorize 4r/(3π) ≈ 0.424r. NOT r/2.

When To Use

Semicircular flanges or cut-outs (e.g., architectural sections)

Formula

Quarter-circle: distance from each straight edge = 4r/(3π)

Meaning

r = radius

Watch Out

Same as semicircle: 4r/(3π) in BOTH x and y directions.

When To Use

Quarter-circle fillets or sections

Common Values

Value

(b/2, h/2)

Symbol

x̄rect, ȳrect

Quantity

Centroid of rectangle from corner

Value

h/3 perpendicular to base

Symbol

ȳtri

Quantity

Centroid of triangle from base

Value

4r / (3π) ≈ 0.424r

Symbol

ȳsemi

Quantity

Centroid of semicircle from diameter

Section Title

Centroid of Composite Areas

Important Facts

  • Centroid is ALWAYS on every axis of symmetry — use this to reduce calculation.
  • Holes (cut-outs) are treated as NEGATIVE areas: subtract both A and coordinates.
  • For symmetric sections (I-beam, channel, angle), one coordinate is zero or obvious by symmetry.
  • Origin location matters: always state the reference point (corner, base, etc.).
  • Centroid does NOT have to be inside the material (e.g., hollow tube or angle section).

Key Definitions

Term

Centroid

Example

A 100×100 mm square has centroid at (50, 50) mm from one corner.

Definition

The geometric center (balance point) of an area, found as the area-weighted average of coordinates.

Term

Composite Area

Example

T-section = rectangle (flange) + rectangle (web); L-section = two rectangles.

Definition

A complex shape made of simple standard shapes (rectangles, triangles, circles) added or subtracted.

Term

Axis of Symmetry

Example

A square has 4 axes of symmetry; the centroid is at the intersection (center).

Definition

A line about which a shape is mirror-symmetric; the centroid always lies on every axis of symmetry.

Diagrams To Know

  • T-section with centroid marked (flange top, web bottom)
  • L-section with divided areas (two rectangles, centroid shown)
  • Composite rectangle with circular hole — centroid shift illustrated
  • Trapezoid divided into simple shapes (rectangle + triangles)

Reactions Or Equations

Note

This is the definition of centroid. Every composite section problem starts here.

Equation

x̄ = Σ(Aᵢ × xᵢ) / ΣAᵢ (same for ȳ with yᵢ)

Conditions

All areas in same unit system; coordinates measured from same origin

Note

Total area is sum of parts minus holes. Used in deflection, stress formulas later.

Equation

Acomposite = ΣAᵢ − Aholes

Conditions

Standard addition/subtraction of areas

Formulas

Formula

Ix = ∫y² dA; Iy = ∫x² dA

Meaning

Ix, Iy = moments of inertia about x and y axes; y, x = perpendicular distances from axis

Watch Out

This is an integral (sum of area elements times squared distance). Don't confuse with first moment (centroid).

When To Use

Definition of moment of inertia. Used to derive standard formulas below.

Formula

Rectangle (about centroidal axis): I = bh³/12

Meaning

b = width parallel to axis, h = depth perpendicular to axis

Watch Out

bh³/12 is about CENTROID. For moment about the base: Ibase = bh³/3. Check your reference point!

When To Use

Any rectangular part of a composite section (transfer with parallel-axis theorem if off-center)

Formula

Rectangle (about base axis): I = bh³/3

Meaning

b = width, h = height from base

Watch Out

Ibase = Icentroid + A(h/2)² = bh³/12 + (bh)(h/2)² = bh³/12 + bh³/4 = bh³/3 ✓

When To Use

Rarely used directly in composite sections (use parallel-axis theorem instead)

Formula

Triangle (about centroidal axis): I = bh³/36

Meaning

b = base width, h = height perpendicular to base

Watch Out

bh³/36 is about CENTROID (at h/3 from base). Not bh³/12.

When To Use

Triangular parts (e.g., trapezoidal section divided into rectangle + triangle)

Formula

Triangle (about base axis): I = bh³/12

Meaning

b = base width, h = height

Watch Out

Ibase = Icentroid + A d² = bh³/36 + (bh/2)(h/3)² = bh³/36 + bh³/18 = bh³/12 ✓

When To Use

Less common (use parallel-axis to shift to centroid if needed)

Formula

Circle (about centroid): I = πd⁴/64 = πr⁴/4

Meaning

d = diameter, r = radius

Watch Out

πd⁴/64 uses diameter. If given radius: πr⁴/4. Both equal; don't mix.

When To Use

Circular sections or holes; same Ix = Iy by symmetry

Formula

Hollow Rectangle: I = (b₁h₁³ − b₂h₂³)/12

Meaning

b₁, h₁ = outer width/height; b₂, h₂ = inner (hole) width/height; centroid shared

Watch Out

Only works if centroids coincide. If off-center: calculate each part separately with parallel-axis.

When To Use

When inner and outer rectangles are concentric (same centroid)

Common Values

Value

bh³/12

Symbol

Irect,c

Quantity

Rectangle centroidal moment

Value

bh³/3

Symbol

Irect,base

Quantity

Rectangle base moment

Value

bh³/36

Symbol

Itri,c

Quantity

Triangle centroidal moment

Value

πd⁴/64 or πr⁴/4

Symbol

Icircle

Quantity

Circle moment

Section Title

Moment of Inertia (Second Moment of Area)

Important Facts

  • Moment of inertia ALWAYS increases with distance from an axis (proportional to distance²).
  • For a given area, SPREAD the material as far as possible from the axis to maximize I (e.g., I-beam flanges far from web).
  • Moment of inertia is NEVER negative; it's always positive and increases with d².
  • Square sections have Ix = Iy; rectangular sections have Iwide > Inarrow (compare to weak axis).
  • Hollow sections (tubes, boxes) have high I-to-weight ratio — preferred in design.

Key Definitions

Term

Moment of Inertia (Second Moment of Area)

Example

A tall, narrow rectangle has large I about its weak axis; a square has equal I in both directions.

Definition

A measure of how an area is distributed about an axis, quantifying resistance to bending and buckling. Units: mm⁴ or m⁴.

Term

Centroidal Axis

Example

For a rectangle, the centroidal x-axis is at y = h/2 from the base.

Definition

An axis passing through the centroid of the shape.

Term

Principal Axes

Example

For a rectangle or T-section, principal axes are usually horizontal and vertical.

Definition

Orthogonal axes about which Imax and Imin occur; for symmetric shapes, they coincide with axes of symmetry.

Diagrams To Know

  • Rectangle with bh³/12 formula applied to centroidal axis
  • Triangle with centroid at h/3, moment arms shown
  • Comparison: same-area rectangle vs. tall narrow rectangle (illustrates I effect)
  • Hollow rectangle with inner/outer boundaries labeled

Reactions Or Equations

Note

This integral is the foundation. AISC 360 and design codes rely on tabulated I values.

Equation

I = ∫y² dA definition; standard formulas derived by integration

Conditions

y measured perpendicular from the axis of interest

Note

This is the parallel-axis theorem. Rearranged, it proves Ibase > Icentroid always.

Equation

Ibase = Icentroid + A(d)² where d = distance from centroid to base

Conditions

Axis parallel to centroidal axis

Formulas

Formula

I = Ī + Ad²

Meaning

I = moment of inertia about any axis; Ī = moment about centroidal axis; A = area; d = distance from centroid to new axis

Watch Out

BIGGEST BOARD MISTAKE: Using only Ī (centroidal) and forgetting Ad². This UNDERESTIMATES I by huge amounts for off-axis parts. The Ad² term is 50%+ of total I for many sections.

When To Use

ALWAYS for composite sections. Every single part needs this transfer to the composite centroid before summing.

Formula

I_composite = Σ(Ī_i + A_i d_i²) − (Ī_holes + A_holes d_holes²)

Meaning

Sum transferred inertias of all parts; subtract holes using NEGATIVE area and NEGATIVE terms

Watch Out

HOLES are negative. If you forget to subtract a hole's Ī AND its Ad² term, you've massively overstated I.

When To Use

Step-by-step procedure for T-sections, I-beams, L-sections, any built-up shape

Common Values

Value

I_base / I_centroid = 3 (for rectangles)

Symbol

Ratio

Quantity

Multiplier for base moment vs centroidal

Value

Depends on geometry; flange ≈ h/3 to h/2 from centroid

Symbol

d

Quantity

Typical d value (T-section example)

Section Title

Parallel-Axis Theorem (THE WORKHORSE)

Important Facts

  • The parallel-axis theorem is the #1 tested skill on the PRC exam for composite sections.
  • You MUST locate the composite centroid FIRST before applying the theorem.
  • Distance d is ALWAYS measured from the PART'S centroid to the COMPOSITE centroid — get the reference right.
  • The Ad² term grows with d². For sections with parts far from the centroid, Ad² often dominates Ī.
  • Forgetting this theorem on an exam results in dramatically incorrect answers (off by 2×, 3×, or more).

Key Definitions

Term

Parallel-Axis Theorem

Example

A rectangle's moment about the base is 5 times larger than about its centroid, due to the Ad² term.

Definition

A method to transfer moment of inertia from a centroidal axis to any parallel axis using I = Ī + Ad².

Term

Composite Section Procedure

Example

T-section: divide into top flange and stem (web). Find composite ȳ. Transfer each part's I to ȳ line. Sum.

Definition

Step 1: Divide into simple parts. Step 2: Find overall centroid (x̄, ȳ). Step 3: For each part, calculate Ī and d (distance from part centroid to composite centroid). Step 4: Apply I = Ī + Ad² and sum.

Diagrams To Know

  • T-section with flange and web separated, showing d (distance from each part centroid to composite ȳ)
  • Rectangle with centroidal axis vs. base axis, Ad² term illustrated
  • L-section with two rectangles, d vectors shown for each, composite centroid marked
  • I-beam with flanges and web, distance from flange centroid to I-beam centroid labeled

Reactions Or Equations

Note

Proven by integration; no exceptions. Always holds. Always use it for composite sections.

Equation

I_axis = I_centroid + A × d²

Conditions

d = perpendicular distance between the two parallel axes

Note

If you shift origins, recalculate d. Common error: inconsistent coordinate systems.

Equation

d = |distance from part centroid to composite centroid|

Conditions

Both centroid locations must be measured from the SAME origin

Formulas

Formula

J = Ix + Iy

Meaning

J = polar moment of inertia; Ix, Iy = moments about perpendicular centroidal axes

Watch Out

J ≠ I about any single axis. J is the SUM of two perpendicular moments. For circles, Ix = Iy, so J = 2I.

When To Use

Torsion problems, circular/symmetric sections. When you need resistance to twisting or overall radius of gyration.

Formula

Circle: J = πd⁴/32 = πr⁴/2

Meaning

d = diameter, r = radius; uses πd⁴/32 or πr⁴/2 (equivalent)

Watch Out

J (polar) is TWICE the I (bending) for a circle. Don't confuse: I = πd⁴/64, but J = πd⁴/32.

When To Use

Solid circular shafts, circular holes, polar moment of circular sections

Formula

Radius of Gyration: r = √(I/A)

Meaning

r = radius of gyration; I = moment of inertia; A = area

Watch Out

r is NOT the same as the physical radius of a shape. It's the equivalent distance if area were concentrated at that radius. Small r → easy to buckle.

When To Use

Column buckling (slenderness ratio λ = L/r), deflection formulas, compact sections per AISC 360

Formula

Slenderness Ratio: λ = L/r (or L/ry for weak axis)

Meaning

L = effective length of column; r = radius of gyration about buckling axis (rmin for critical)

Watch Out

Use MINIMUM radius of gyration (rmin = √(Imin/A)). High λ → slender → low buckling capacity.

When To Use

Column stability check per NSCP 2015, AISC 360 (Euler/Johnson buckling formulas)

Formula

Rectangular section: rx = h/√12 ≈ 0.289h (about weak axis)

Meaning

h = dimension perpendicular to weak axis

Watch Out

For a rectangle, rx ≠ ry unless it's a square. Use minimum (weak axis) for buckling.

When To Use

Quick check for slenderness of a column with rectangular cross-section

Common Values

Value

r = h / √12 ≈ 0.289h

Symbol

rmin

Quantity

Radius of gyration: rectangle (weak axis)

Value

J = πd⁴/32

Symbol

Jcircle

Quantity

Polar moment: circle

Value

λ ≤ 200 (recommended); λ > 300 very slender

Symbol

λ

Quantity

Typical slenderness limit (NSCP/AISC)

Section Title

Polar Moment & Radius of Gyration

Important Facts

  • For circles: Ix = Iy (by symmetry), so J = 2I.
  • For rectangles: Ix ≠ Iy (one is 'strong,' one is 'weak' axis); minimum r governs column buckling.
  • Slenderness ratio λ = L/r directly appears in AISC 360 buckling formulas (Euler: Fcr = π²E/(λ)²).
  • NSCP 2015 §5.7.3 (Column Design) uses λ = KL/r where K is the effective length factor (K=1 for pinned ends).
  • Compact/non-compact section classification per AISC 360 §B4 depends on width-to-thickness ratios, not on r directly, but r is critical for slenderness checks.

Key Definitions

Term

Polar Moment of Inertia

Example

For a circular shaft, J = πd⁴/32 governs torque capacity.

Definition

The sum of moments of inertia about two perpendicular centroidal axes; measures resistance to twisting (torsion).

Term

Radius of Gyration

Example

A column with small r buckles easily; one with large r resists buckling.

Definition

An equivalent distance from an axis at which the entire area could be concentrated to produce the same moment of inertia. Units: mm or m.

Term

Slenderness Ratio

Example

λ > 200 is typically very slender; λ < 50 is relatively stocky.

Definition

The dimensionless ratio λ = L/r; a measure of how slender (prone to buckling) a column is.

Diagrams To Know

  • Circle with Ix = Iy marked, showing J = 2I
  • Rectangle with rx (weak) and ry (strong) axes, rx shown smaller
  • Column with height L and cross-section showing r, slenderness ratio λ = L/r illustrated
  • Buckling modes (Euler) with slenderness effect on failure load

Reactions Or Equations

Note

For circles: J = πd⁴/32. For rectangles: J = Ix + Iy; usually calculated from known Ix, Iy.

Equation

J = Ix + Iy (perpendicular-axis theorem for centroidal axes)

Conditions

Ix and Iy are about perpendicular centroidal axes

Note

Sometimes exam asks for I given r and A; sometimes for r given I and A. Know both forms.

Equation

r = √(I/A) or equivalently I = r² A

Conditions

Rearrangeable; useful in both directions

Note

Slenderness governs Euler vs Johnson buckling curve selection.

Equation

λ = L/r or λ_max = L/rmin (use minimum radius for buckling)

Conditions

For pinned ends (K=1); for other end conditions, use λ = KL/r per AISC/NSCP

Common Values

Value

A ≈ 33.7 cm², Ix ≈ 1943 cm⁴, Iy ≈ 164 cm⁴, rx ≈ 8.57 cm, ry ≈ 2.21 cm

Symbol

Properties (from manual)

Quantity

IPB 200×100 (example)

Value

A ≈ 60.3 cm², Ix = Iy ≈ 2345 cm⁴ (symmetric), r ≈ 6.23 cm

Symbol

Properties (from manual)

Quantity

Hollow Box 200×200×8 (example)

Section Title

Standard Section Centroid & Inertia Values (Quick Lookup)

Important Facts

  • AISC 360 (US) and Philippine structural steel manuals (e.g., Philippine National Steel Corp tables) tabulate Ix, Iy, rx, ry for standard shapes.
  • Common Philippine/regional I-beam sizes: IPB (universal beam) 100×55 to 600×210 mm; values tabulated in design handbooks.
  • Channels (C-shapes) and Angles (L-shapes) are asymmetric; their Ix ≠ Iy; centroid is NOT at geometric center.
  • Hollow rectangular (box) and circular (pipe) sections: look up or use outer − inner formula (if concentric).
  • Design codes (NSCP 2015 Section 5) reference these tabulated values directly; always confirm your section from a reputable source.

Diagrams To Know

  • Standard I-beam profile with centroid and principal axes labeled
  • Channel (C-section) with centroid offset from geometric center
  • Angle (L-section) with principal axes rotated (not aligned with edges)
  • Hollow box section with outer and inner rectangles

Must Remember

  • PARALLEL-AXIS THEOREM: I = Ī + Ad². This is the #1 tested formula. EVERY composite section requires this. Forgetting Ad² underestimates I by 2–3×.
  • CENTROID FORMULA: x̄ = ΣAᵢxᵢ / ΣAᵢ (area-weighted average). HOLES are NEGATIVE areas — subtract both A and coordinates. Get this wrong, entire solution fails.
  • RECTANGLE CENTROID I: bh³/12 (CENTROID), NOT bh³/3 (base). The base formula = bh³/3. Know which axis you're using.
  • TRIANGLE CENTROID: h/3 from base (NOT h/2). Memorize 1/3, not 1/2. Same for moment: Ī = bh³/36, NOT bh³/12.
  • CIRCLES: Bending I = πd⁴/64. Polar moment J = πd⁴/32 (TWICE the bending I). Moment about base axis: πd⁴/64 (circles always centered at centroid anyway).
  • RADIUS OF GYRATION: r = √(I/A). Governs slenderness λ = L/r (column buckling per NSCP 2015 §5.7.3). Small r → easy to buckle. Use MINIMUM radius for buckling.
  • COMPOSITE SECTIONS STEP-BY-STEP: (1) Divide into simple shapes. (2) Find composite centroid. (3) Calculate Ī for each part. (4) Find d (part centroid to composite centroid). (5) Transfer: I = Ī + Ad². (6) Sum. Missing any step = wrong answer.
  • AXIS OF SYMMETRY: Centroid always lies on every axis of symmetry. Use this to eliminate unknowns (e.g., if symmetric about y-axis, then x̄ is obvious).
  • T-SECTION TRAP: Flange and web have different centroids. You MUST calculate the composite ȳ first, then apply parallel-axis theorem to BOTH parts (not just the web).
  • HOLES ARE NEGATIVE: When calculating x̄, ȳ, A, Ī for a section with holes: subtract area, subtract coordinates, subtract (transferred) inertia. One forgotten negative term ruins the whole answer.

Last Minute Tips

  • Always state your origin and reference axes explicitly (e.g., 'measuring from bottom-left corner'). Misaligned coordinates kill composite centroid calculations.
  • For T-, I-, and L-sections: divide into TWO parts (flange/web or two legs), NOT three or four. This reduces error and matches the exam format.
  • Check dimension units: if section is in mm, your Ī will be in mm⁴. If problem wants m⁴, convert by (10³)⁴ = 10¹². Don't forget unit conversion in final answer.
  • The parallel-axis theorem Ad² term often exceeds Ī by 2–3× for off-center parts. If your Ad² looks small compared to Ī, re-check your calculation (likely d is too small).
  • For columns (NSCP 2015 §5.7): always use rmin (= √(Imin/A)), not rmax. Using weak-axis moment of inertia ensures conservative buckling check. Using strong-axis r will underestimate buckling risk.

Comparison Tables

Rows

Values

  • Ix = bh³/12
  • Shortest distance from part of section to axis is h/2
  • Base for parallel-axis theorem; used to find moment about any parallel axis

Property

About Centroid

Values

  • Ix = bh³/3
  • Longest distance from bottom of section is h; Ad² = (bh)(h/2)² adds 2 × centroidal moment
  • Rarely used directly; always convert via parallel-axis theorem in composite sections

Property

About Base

Values

  • Ibase = Icentroid + A(h/2)²
  • bh³/3 = bh³/12 + bh(h²/4) = bh³/12 + bh³/4 = bh³/3 ✓
  • This IS the parallel-axis theorem: I = Ī + Ad²

Property

Relationship

Columns

  • Axis
  • Formula
  • Why Different
  • Usage

Table Title

Moment of Inertia Formulas: Centroid vs. Base (Rectangle)

Rows

Values

  • (b/2, h/2)
  • At the geometric center; halfway in both directions

Property

Rectangle

Values

  • (b/3, h/3) from right angle vertex
  • One-third along each leg; NOT at h/2

Property

Triangle (right angle at origin)

Values

  • 4r/(3π) ≈ 0.424r from diameter
  • Closer to the curved side; 4r/(3π), NOT r/2

Property

Semicircle

Values

  • 4r/(3π) from EACH straight edge
  • Same formula both x and y directions from the right-angle corner

Property

Quarter-circle

Columns

  • Shape
  • Centroid Location
  • Memo

Table Title

Common Shape Centroid Locations (from reference edge)

Rows

Values

  • I = bh³/12
  • b parallel to axis; h perpendicular
  • Using bh³/3 (base formula) instead; or confusing b and h direction

Property

Rectangle

Values

  • I = bh³/36
  • Centroid at h/3 from base; one-third of rectangle's I
  • Using bh³/12 (base formula); or h/2 instead of h/3

Property

Triangle

Values

  • I = πd⁴/64 = πr⁴/4
  • Ix = Iy by symmetry; J = 2I
  • Using πd⁴/32 (polar, which is J not I); or confusing diameter and radius

Property

Circle

Values

  • I = (b₁h₁³ − b₂h₂³)/12
  • Outer − inner; both measured from shared centroid
  • Using if centroids do NOT coincide (must use parallel-axis theorem instead)

Property

Hollow Rect (concentric)

Columns

  • Shape
  • Moment Formula
  • Key Note
  • Common Mistake

Table Title

Moment of Inertia Formulas by Shape (Centroidal Axis)

Rows

Values

  • Split into simple shapes (flange, web)
  • Using overlapping regions instead of non-overlapping parts

Property

1. Divide Section

Values

  • Use x̄ = ΣAixī / ΣAi and ȳ = ΣAiyī / ΣAi
  • Wrong origin; forgetting to subtract hole contributions; sign error on hole coordinates

Property

2. Find Composite Centroid

Values

  • For each part, find Ī (about part centroid) using standard formula
  • Using formula for wrong axis (base vs. centroid); confusing centroid location of the part

Property

3. Calculate Part Inertias

Values

  • d = distance from PART centroid to COMPOSITE centroid
  • Measuring from wrong reference; inconsistent origin; forgetting magnitude (use |d|)

Property

4. Find Distances d

Values

  • For each part, calculate transferred moment; sum all parts
  • Forgetting the Ad² term entirely (underestimates I by 50%+); wrong sign on holes

Property

5. Apply I = Ī + Ad²

Columns

  • Step
  • Action
  • Common Error

Table Title

Parallel-Axis Theorem Application: T-Section Example Checklist

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