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CELE Engineering MechanicsEquilibrium of Particles and Rigid BodiesStudy Notes

Full study notes for Equilibrium of Particles and Rigid Bodies — built specifically for the CELE 2026. These notes cover every concept, definition, formula, and worked example you need for the Engineering Mechanics subtest of the CELE, structured in the order Professional Regulation Commission (PRC) — Board of Civil Engineering typically tests them.

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. Equilibrium of Particles and Rigid Bodies lands at position 2nd 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.

Equilibrium of Particles and Rigid Bodies - Study Notes

Equilibrium is the foundational principle of structural analysis and design in civil engineering. A body is in equilibrium when the net force and net moment acting on it are zero—it neither accelerates linearly nor rotates. This concept underpins every structural design from simple beams to complex frames. For the Professional Civil Engineer (PCE) examination under RA 544, mastery of equilibrium analysis using free-body diagrams and the equilibrium equations is essential. This chapter covers particle equilibrium, including Lami's theorem; rigid-body equilibrium with support reactions; two-force and three-force members; and practical applications aligned with NSCP 2015 design standards.

Summary

Equilibrium is the cornerstone of structural analysis. A body in equilibrium has zero net force and zero net moment. This chapter covered the three equilibrium equations (ΣFₓ = 0, ΣFᵧ = 0, ΣM = 0), the critical importance of free-body diagrams, particle equilibrium (with Lami's Theorem for three concurrent forces), and rigid-body equilibrium (including support reactions and the strategic choice of moment points). Two-force members (like truss members) carry force along their axis only; three-force members are in equilibrium only if the forces are concurrent or parallel—these properties enable quick problem-solving and verification. Support types define available reactions: rollers provide 1, pins provide 2, fixed ends provide 3 (in 2D). Distributed loads must be converted to resultants at their centroids. The chapter also introduced statically indeterminate systems (more unknowns than equations) and 3D equilibrium (six equations, six unknowns possible). Common exam pitfalls include wrong support reactions, misplaced distributed load resultants, Lami angle errors, and sign confusion. Mastery of these concepts is essential for the PCE examination and for all subsequent structural analysis and design work. Every beam analysis, every joint in a frame, every truss member check starts with equilibrium—get it right, and the rest follows.

Sections

Equilibrium occurs when a body is at rest or moving with constant velocity—that is, when acceleration is zero. Newton's First Law forms the basis: a body remains in its state of motion unless acted upon by an unbalanced force. In structural engineering, we typically deal with static equilibrium—the body is at rest. For a body in two-dimensional (2D) equilibrium, three conditions must be satisfied: • Sum of forces in the x-direction equals zero: ΣFₓ = 0 • Sum of forces in the y-direction equals zero: ΣFᵧ = 0 • Sum of moments about any point equals zero: ΣM = 0 These three independent equations allow us to solve for a maximum of three unknowns in a 2D problem. In three-dimensional (3D) problems, we have six equations (three force, three moment) and can solve up to six unknowns. The key principle is that we can take moments about ANY point and get the same result. Smart engineers choose the moment point strategically—often at a support location where unknown reactions pass through, eliminating those unknowns from the equation and simplifying the solution. This is not a trick; it is the correct application of the moment equation.

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1. Fundamental Principles of Equilibrium

Examples

Understanding Moment Point Selection

A simply supported beam AB, 6 m long, carries a 50 kN downward load at 2 m from A. If we sum moments about point A, the reaction at A does not appear (arm = 0). If we sum moments about point B, the reaction at B does not appear. Choosing the correct point reduces algebra.

Worked Solution

Taking moments about A: R_B × 6 = 50 × 2 → R_B = 16.67 kN. Taking moments about B would give: R_A × 6 = 50 × 4 → R_A = 33.33 kN. Both yield correct answers; the choice is purely for convenience.

Key Points

  • Equilibrium requires ΣFₓ = 0, ΣFᵧ = 0, and ΣM = 0 in 2D systems
  • The three equilibrium equations are independent and provide exactly three equations for three unknowns
  • The moment equation can be applied about any point; choose wisely to simplify calculations
  • Static equilibrium means the body is at rest; there is no acceleration or rotation
  • Moment summation eliminates unknown forces that lie on the chosen point, a powerful problem-solving strategy

A free-body diagram is a sketch of the isolated body showing every external force acting on it. It is the single most critical step in equilibrium analysis. An incorrect FBD leads to wrong answers no matter how perfectly the equations are solved. When drawing an FBD: 1. **Isolate the body** — mentally separate it from its surroundings. 2. **Show all applied loads** — point loads, distributed loads (as resultants), couples, self-weight if significant. 3. **Replace supports with reactions** — do not draw the supports themselves; show the forces and moments they exert: - **Roller support**: One reaction perpendicular to the surface (normal direction only). No friction assumed unless stated. - **Pin support (hinge)**: Two reactions—horizontal (Hₓ) and vertical (Hᵧ). The pin prevents translation in both directions but allows rotation. - **Fixed support (encastrement)**: Three reactions—horizontal (Hₓ), vertical (Vᵧ), and a moment (M). The fixed end prevents both translation and rotation. - **Built-in cantilever**: Same as fixed support. 4. **Show directions** — assume a positive direction (usually rightward for horizontal, upward for vertical). If the actual direction is opposite, the calculated value will be negative. 5. **Label dimensions and magnitudes** — ensure all geometry and load values are clear. Common mistakes: - Drawing the support structure instead of just the reactions it provides. - Forgetting a load (especially self-weight or horizontal components). - Assuming a wrong support type (many students confuse pin and roller). - Drawing reactions in the wrong direction—guess an initial direction, and let the math reveal the true direction.

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2. Free-Body Diagram (FBD)—The Foundation of Analysis

Examples

Identifying Support Types and Reactions

A horizontal beam rests on a brick wall (left end, fixed) and is supported by a cable to a pulley (right end, roller on a horizontal surface). A downward 100 kN load acts at mid-span.

Worked Solution

Left support (fixed wall): Draws Hₗ, Vₗ, and Mₗ. Right support (roller): Draws Vᵣ only, acting upward perpendicular to the horizontal surface. Applied load: 100 kN downward at mid-span. This FBD has three unknowns (Hₗ, Vₗ, Mₗ) plus Vᵣ = 4 unknowns. But the cable is horizontal and provides no vertical component, so Hₗ is typically zero unless wind acts. Thus ΣFₓ = 0 yields Hₗ = 0 (or equals horizontal cable tension if present).

Distributed Load Replacement

A simply supported beam, 8 m long, carries a trapezoidal distributed load: 10 kN/m at the left, 20 kN/m at the right.

Worked Solution

For moment calculations, the trapezoidal load must be split or integrated, or viewed as the sum of a triangular load (centroid at 5.33 m from left, resultant = 40 kN) plus a rectangular load (centroid at 4 m, resultant = 80 kN). Total = 120 kN; combined centroid at (40 × 5.33 + 80 × 4)/(120) = 4.44 m from left. Use this single point for moments.

Key Points

  • An FBD must show the isolated body with every external force and moment
  • Supports must be replaced by their reaction forces and moments, not drawn as structures
  • A roller provides 1 reaction (perpendicular to surface); a pin provides 2 (Hₓ, Vᵧ); a fixed end provides 3 (Hₓ, Vᵧ, M)
  • Always assume positive directions and let the calculations reveal the true direction
  • A poor FBD guarantees a poor solution, regardless of mathematical skill
  • For distributed loads, replace with the resultant force at the centroid before solving

A **particle** is a body whose physical dimensions are negligible compared to the distances involved, or more practically, all forces act at a single point (concurrent forces). For a particle, only translational equilibrium matters; there is no rotation to worry about. Thus: ΣFₓ = 0 and ΣFᵧ = 0 (only two equations; no moment equation) When exactly three concurrent forces hold a particle in equilibrium and no other forces act, **Lami's Theorem** provides a powerful shortcut. Lami's Theorem states: F₁/sin(α₁) = F₂/sin(α₂) = F₃/sin(α₃) where each angle αᵢ is the angle **between the other two forces**, not the angle from a reference axis. **Why Lami works:** The three forces form a closed triangle when drawn tip-to-tail (vector polygon). The sine rule for triangles directly applies to this polygon. **When to use Lami:** - Exactly three concurrent forces. - At least one force is fully known (magnitude and direction). - Directions of all three forces are known. - Solving manually without a computer. **Angle identification is critical.** If forces F₁, F₂, F₃ meet at a point, the angle α₁ is the angle **between F₂ and F₃** (the angle at the corner where F₁ points away). This is the common mistake: students often use the exterior angle or the angle from a reference direction. **Common setup:** A weight hangs from a point held by two cords or cables at different angles to horizontal/vertical supports. The three forces are: (1) tension in cord 1, (2) tension in cord 2, (3) weight (known, downward).

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3. Particle Equilibrium and Lami's Theorem

Examples

Hanging Weight with Two Cords—Lami Application

A 600 N weight hangs from a point. Cord 1 goes to the left wall at 60° above horizontal. Cord 2 goes to the right wall at 30° above horizontal. Find both tensions.

Worked Solution

Three forces: T₁ (left, unknown), T₂ (right, unknown), W = 600 N (downward, known). Angle between T₂ and W: The angle at the vertex where T₁ acts. Cord 2 is 30° above horizontal (slopes down-right), weight is vertical down. The angle between them is 90° − 30° = 60°. So α₁ = 60°. Angle between T₁ and W: The angle at the vertex where T₂ acts. Cord 1 is 60° above horizontal (slopes down-left), weight is vertical down. The angle between them is 90° − 60° = 30°. So α₂ = 30°. Angle between T₁ and T₂: They point in opposite horizontal directions, both upward. The angle between them is 60° + 30° = 90° at the junction? No—visualize: Cord 1 is 60° up from horizontal-left, Cord 2 is 30° up from horizontal-right. The angle between them (interior angle at the hanging point) is 180° − 60° − 30° = 90°. So α₃ = 90°. Apply Lami: T₁/sin(α₁) = T₂/sin(α₂) = W/sin(α₃) T₁/sin(60°) = T₂/sin(30°) = 600/sin(90°) T₁/0.866 = T₂/0.5 = 600/1 T₁ = 600 × 0.866 = 519.6 N T₂ = 600 × 0.5 = 300 N Verification (components): ΣFₓ = −519.6 cos(60°) + 300 cos(30°) = −259.8 + 259.8 = 0 ✓ ΣFᵧ = 519.6 sin(60°) + 300 sin(30°) − 600 = 450 + 150 − 600 = 0 ✓

Three Cables at a Junction—When Lami Applies

Three cables meet at a point: one goes to an anchor 45° below horizontal to the right (tension T₁, unknown); one goes to an anchor 60° above horizontal to the left (tension T₂, unknown); one carries a 500 N load downward (T₃ = 500 N, known). Find T₁ and T₂.

Worked Solution

Identify the angle between each pair: - Between T₂ (60° above horizontal-left) and T₃ (straight down): The angle is 60° + 90° = 150°. So α₁ = 150°. - Between T₁ (45° below horizontal-right) and T₃ (straight down): The angle is 45° + 90° = 135°. So α₂ = 135°. - Between T₁ and T₂: From 45° below horizontal-right to 60° above horizontal-left is 45° + 180° − 60° = 165°? No, interior angle: 45° + 60° + (angle to vertical) = ... Better: use 360° − 150° − 135° = 75°. So α₃ = 75°. Apply Lami: T₁/sin(150°) = T₂/sin(135°) = 500/sin(75°) T₁/0.5 = T₂/0.7071 = 500/0.9659 T₁ = (500/0.9659) × 0.5 = 258.8 N T₂ = (500/0.9659) × 0.7071 = 366.0 N

Key Points

  • A particle has all forces acting at one point (concurrent); only ΣFₓ = 0 and ΣFᵧ = 0 apply
  • Lami's Theorem applies only when exactly three forces are in equilibrium
  • Each angle in Lami's Theorem is between the other two forces, not from a reference axis
  • Lami is faster than component equations for three-force problems but requires correct angle identification
  • The vector polygon (three forces drawn tip-to-tail) closes when in equilibrium; the sine rule applies to this polygon

A **rigid body** is one whose shape does not deform under load (an idealization; real materials deform slightly, but we often ignore it). Unlike particles, rigid bodies can rotate, so all three equilibrium equations apply: ΣFₓ = 0, ΣFᵧ = 0, ΣM = 0. **General procedure for solving support reactions:** 1. **Draw the free-body diagram** with all applied loads and support reactions. 2. **Count unknowns** and confirm that there are at most three (for 2D): - Simply supported beam (pin + roller) = 3 unknowns ✓ - Cantilever (fixed end) = 3 unknowns ✓ - Two pins (overconstrained without knowing member internal forces) = typically statically indeterminate without additional information 3. **Apply the moment equation** about a strategic point (usually a support) to eliminate unknown reactions at that point and solve for a reaction at another support. 4. **Apply force equations** to find remaining unknowns. 5. **Check** using a third equation (e.g., if moments were taken about the left support, verify with moments about the right support or with the sum of forces). **Distributed load conversion:** A uniformly distributed load (UDL) of intensity q (kN/m) over length L becomes a resultant force F = q × L, acting at the centroid of the load region (L/2 from either end for uniform). For non-uniform distributions (triangular, trapezoidal), locate the centroid by geometry or integration. **Inclined loads and reactions:** Decompose inclined forces into horizontal and vertical components before applying equilibrium equations. **Sign convention:** Assume positive directions (e.g., right is +x, up is +y, counterclockwise is +M). If the calculated value is negative, the force/moment is opposite to the assumed direction. This is **not** an error; it is the correct interpretation.

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4. Equilibrium of Rigid Bodies—Support Reactions

Examples

Simply Supported Beam with Point Load and Distributed Load

Beam AB, length 6 m, simply supported (pin at A, roller at B). A 50 kN downward point load acts at 2 m from A. A uniform distributed load of 20 kN/m acts over the right 3 m (from x = 3 m to x = 6 m). Find all three reactions.

Worked Solution

FBD: - At A (pin): Horizontal reaction Aₓ, vertical reaction Aᵧ (both unknown). - At B (roller): Vertical reaction Bᵧ (upward, unknown). - Applied: 50 kN downward at x = 2 m; UDL 20 kN/m from x = 3 to 6 m. Converted UDL: Magnitude = 20 × 3 = 60 kN, acting at x = (3 + 6)/2 = 4.5 m from A. Apply ΣM_A = 0 (moments about A, taking counterclockwise as positive): Bᵧ(6) − 50(2) − 60(4.5) = 0 6Bᵧ = 100 + 270 = 370 Bᵧ = 61.67 kN (upward) Apply ΣF_y = 0: Aᵧ + Bᵧ − 50 − 60 = 0 Aᵧ = 110 − 61.67 = 48.33 kN (upward) Apply ΣF_x = 0: Aₓ = 0 (no horizontal applied forces) Check with ΣM_B = 0: Aᵧ(6) − 50(4) − 60(1.5) = 48.33(6) − 200 − 90 = 290 − 290 = 0 ✓ Final answers: Aₓ = 0, Aᵧ = 48.33 kN, Bᵧ = 61.67 kN.

Cantilever Beam with Fixed-End Reactions

A cantilever beam, 3 m long, fixed at the left end A and free at the right end B. A 20 kN downward point load acts at B. A uniform load of 5 kN/m acts over the entire length. Find the fixed-end reactions.

Worked Solution

FBD: - At A (fixed): Horizontal reaction Aₓ, vertical reaction Aᵧ, and reaction moment M_A (all unknown). - Applied: 20 kN downward at x = 3 m (end B); UDL 5 kN/m over entire 3 m. Converted UDL: Magnitude = 5 × 3 = 15 kN, acting at x = 3/2 = 1.5 m from A. Apply ΣF_y = 0: Aᵧ − 20 − 15 = 0 Aᵧ = 35 kN (upward) Apply ΣF_x = 0: Aₓ = 0 (no horizontal loads) Apply ΣM_A = 0 (moments about the fixed end, counterclockwise positive): M_A − 20(3) − 15(1.5) = 0 M_A = 60 + 22.5 = 82.5 kN·m (counterclockwise, or into the page if we define upward as right-hand rule out of page) Final answers: Aₓ = 0, Aᵧ = 35 kN, M_A = 82.5 kN·m.

Beam with Overhang and Inclined Load

A beam AC, 8 m total length, is simply supported at A (pin) and B (roller at 6 m from A). An overhang extends from B to C (2 m). An inclined load of 100 kN at 30° below horizontal acts at C, pointing down and to the right. Find the reactions at A and B.

Worked Solution

FBD: - At A (pin): Aₓ, Aᵧ (both unknown). - At B (roller): Bᵧ (upward, unknown). - Applied: 100 kN at 30° below horizontal at C (2 m past B). - Horizontal component: 100 cos(30°) = 86.6 kN (to the right). - Vertical component: 100 sin(30°) = 50 kN (downward). Apply ΣM_A = 0: Bᵧ(6) − 100 sin(30°)(8) − 100 cos(30°)(0) = 0 Note: The horizontal component passes through A's height (lever arm = 0 if A is the pivot level), so only the vertical component contributes. Bᵧ(6) = 50(8) = 400 Bᵧ = 66.67 kN (upward) Apply ΣF_y = 0: Aᵧ + Bᵧ − 50 = 0 Aᵧ = 50 − 66.67 = −16.67 kN This negative value means Aᵧ is actually 16.67 kN downward (the overhang pulls the beam down at A). Apply ΣF_x = 0: Aₓ + 86.6 = 0 Aₓ = −86.6 kN The negative sign indicates the reaction is to the left (opposite the applied horizontal load direction, which makes sense—the support opposes the applied load). Interpretation: Aₓ = 86.6 kN to the left, Aᵧ = 16.67 kN downward, Bᵧ = 66.67 kN upward.

Key Points

  • Rigid bodies require all three equilibrium equations: ΣFₓ = 0, ΣFᵧ = 0, ΣM = 0
  • Always draw the FBD first; identify all support types and unknown reactions
  • Take moments about a support point to eliminate unknown reactions and solve for others
  • Convert distributed loads to resultant forces at the centroid before solving
  • Decompose inclined loads into components; handle horizontal and vertical separately
  • Negative calculated values indicate the reaction is opposite to the assumed direction—still correct
  • Three unknowns in 2D; six unknowns in 3D (six equilibrium equations available)

Understanding the geometry of force systems on members provides powerful shortcuts for finding unknown directions or verifying solutions. **Two-Force Member:** A rigid body subjected to forces at only two points is called a two-force member. For equilibrium, the two forces must be equal in magnitude, opposite in direction, and collinear (lie on the same line). The line of action is the straight line connecting the two points of application. **Consequence:** A two-force member can only carry tension or compression along its axis; it cannot carry shear or bending. This is why **truss members** are analyzed as two-force elements—they are long, slender members pinned at the ends, and no load is applied between the pins. Each member carries force along its length only. **Implication for problem-solving:** If you know a member is two-force, you immediately know the direction of the force (along the member). If the member is inclined at angle θ to horizontal, the force is also inclined at θ. This eliminates the need to solve for the direction separately. **Three-Force Member:** A rigid body subjected to three forces is in equilibrium only if (1) the three forces are **concurrent** (all pass through a single point) or (2) the three forces are **parallel**. If the forces are not concurrent and not parallel, the body cannot be in equilibrium. **Consequence:** If two of the three forces are known, the direction of the third force is determined. The line of action of the third force must pass through the intersection point of the lines of action of the other two forces (if concurrent) or be parallel to them. **Implication for problem-solving:** If a member carries three forces and two directions are known, find the intersection point of the first two forces' lines of action. The third force must act along the line connecting this intersection point to the point of application of the third force. **Practical example in frames:** A horizontal beam loaded at mid-span and supported by a pin at one end and a cable at the other. The beam carries three forces: the applied load, the pin reaction, and the cable tension. If the load is vertical and the cable is inclined, the pin reaction direction is determined by the concurrency condition.

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5. Two-Force and Three-Force Members

Examples

Truss Member as a Two-Force Element

A truss member AB is pinned at both ends A and B. An external load P is applied at a point between A and B (e.g., a roof load). Does this member remain two-force?

Worked Solution

No. A load applied between the pins means the member now carries three forces: the pin reaction at A, the pin reaction at B, and the external load P. It is no longer a two-force member. If the load is significant, the member must resist bending and shear, not just axial force. In practice, truss members carry no intermediate loads; all loads are applied only at the joints (pins). If a roof load is applied between joints, the roof deck itself becomes another member sharing the load, or the local panel is analyzed separately as a multi-force element.

Three-Force Member—Beam with Pin and Cable Support

A horizontal beam, 4 m long, is pinned at A (left end) and supported by a cable at B (right end, inclined at 45° above horizontal to an anchor). A vertical load of 100 kN acts at the center (2 m from A). Find the directions of the pin reaction and the cable tension, then verify they are concurrent.

Worked Solution

Three forces on the beam: (1) pin reaction at A (direction unknown), (2) cable tension at B (direction known: 45° above horizontal, along the cable), (3) applied load at the center (direction known: vertical downward, 100 kN). For three-force equilibrium, these must be concurrent. Find the intersection point of the known forces: - Applied load: vertical line through the center (2 m from A). - Cable tension: line at 45° through B (4 m from A). Intersection of these lines: The vertical line x = 2 m and the line y = 45° starting from (4, 0). Line equation: y − 0 = tan(45°) × (x − 4) = (x − 4). At x = 2: y = 2 − 4 = −2 m. This intersection is 2 m below the right support, which is physically above the beam (does the math show the lines intersect above or below the structure?). Rethink: The cable pulls upward and to the right from B (at 45° above horizontal-right). The load pulls downward at x = 2. The vertical line (load) and the 45° line (cable) meet where (x − 4) = y, so at x = 2, y = −2. This means 2 m vertically below point B (which is on the beam). Since the beam is horizontal, this point is geometrically below the structure. For three-force equilibrium, the pin reaction at A must also pass through this point. Line from A (0, 0) to the intersection (2, −2) has slope −2/2 = −1, so the angle is −45° (or 45° below horizontal). The pin reaction magnitude and direction can now be found from the force polygon or component equations. Verification: ΣF_x = A_x + T cos(45°) = 0 and ΣF_y = A_y + T sin(45°) − 100 = 0, where the pin reaction (A_x, A_y) must be collinear with the direction found (−45°). Solving: T = 100/sin(45°) = 141.4 kN, A_x = −141.4 cos(45°) = −100 kN, A_y = −141.4 sin(45°) + 100 = −100 kN. So the pin reaction is 100√2 ≈ 141.4 kN at −135° (or 45° below horizontal-left), which lies on the line from A to the intersection point ✓

Key Points

  • A two-force member carries force along the line joining its two force points; no shear or bending
  • Truss members are two-force members; each carries tension or compression along its axis
  • A three-force member is in equilibrium only if the three forces are concurrent or all parallel
  • For a three-force member, if two force directions are known, the third is determined by the concurrency condition
  • Finding the intersection of two force lines of action gives the direction of the third force in a three-force member
  • These principles allow quick verification of solutions and direct determination of unknown directions

Three-dimensional equilibrium extends the principles of 2D equilibrium to space. A body in 3D is in equilibrium when: ΣFₓ = 0, ΣFᵧ = 0, ΣFᵤ = 0 (three force equations) ΣMₓ = 0, ΣMᵧ = 0, ΣMᵤ = 0 (three moment equations) This gives six independent equations, allowing us to solve for up to six unknowns. **3D Support Types:** 1. **Roller on a plane:** One reaction perpendicular to the plane (e.g., bearing on the ground provides normal force only, not friction or shear unless explicitly stated). 2. **Smooth surface contact:** One reaction normal to the surface. 3. **Pin joint (3D hinge):** Two reactions (perpendicular to the hinge axis). If hinged about the z-axis, reactions are Fₓ and Fᵧ; moment about z is zero, but Mₓ and Mᵧ may be non-zero in a 3D frame. 4. **Ball joint (spherical hinge):** Three reactions (Fₓ, Fᵧ, Fᵤ), allowing rotation in all directions. 5. **Fixed support (encastrement):** Three force reactions (Fₓ, Fᵧ, Fᵤ) and three moment reactions (Mₓ, Mᵧ, Mᵤ). 6. **Slider on a rod:** Prevents motion perpendicular to the rod but allows sliding along the rod. Reactions perpendicular to the rod axis (two reactions if the rod is along z, reactions are Fₓ and Fᵧ). **3D Moment Calculation:** Moment is the cross product: **M** = **r** × **F**, where **r** is the position vector from a reference point to the point of force application, and **F** is the force vector. Mₓ = rᵧFᵤ − rᵤFᵧ Mᵧ = rᵤFₓ − rₓFᵤ Mᵤ = rₓFᵧ − rᵧFₓ **Approach:** Set up a 3D coordinate system, express all force and position vectors in component form, apply the six equilibrium equations, and solve the system (often using matrix algebra or substitution). **Caution:** 3D problems are algebraically intensive. Careful setup and systematic organization are essential. A mistake in signs or coordinates propagates quickly.

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6. Equilibrium in Three Dimensions

Examples

3D Supported Beam with Inclined Load

A beam AB, 5 m long, lies along the x-axis with A at the origin and B at (5, 0, 0). It is supported at A by a ball joint (allowing rotation in all directions) and at B by a roller on the xy-plane (preventing z-motion only, allowing x and y motion). A force of 200 N acts at the center of the beam (x = 2.5 m), directed at 30° below the xy-plane in the yz-plane (i.e., the force has components in y and z, no x-component). Find all six reactions.

Worked Solution

Setup: A at origin with ball joint (Aₓ, Aᵧ, Aᵤ); B at (5, 0, 0) with roller (Bᵤ only, no Bₓ or Bᵧ). Applied force at (2.5, 0, 0): The force is in the yz-plane at 30° below horizontal. Magnitude 200 N. Fₓ = 0 Fᵧ = 200 cos(30°) = 173.2 N Fᵤ = −200 sin(30°) = −100 N (downward/negative z) Force equations: ΣFₓ = Aₓ + 0 = 0 → Aₓ = 0 ΣFᵧ = Aᵧ + 173.2 = 0 → Aᵧ = −173.2 N ΣFᵤ = Aᵤ + Bᵤ − 100 = 0 → Aᵤ + Bᵤ = 100 Moment equations (about point A, x-axis component): ΣMₓ = (r_B × R_B)ₓ + (r_load × F)ₓ = 0 where r_B = (5, 0, 0), R_B = (0, 0, Bᵤ) so (r_B × R_B) = (5, 0, 0) × (0, 0, Bᵤ) = (0, −5Bᵤ, 0). And r_load = (2.5, 0, 0), F = (0, 173.2, −100) so (r_load × F) = (2.5, 0, 0) × (0, 173.2, −100) = (0, 250, 432.5). ΣMₓ = 0 + 0 = 0 ✓ (automatically satisfied) Moment equations (y-axis component): ΣMᵧ = (r_B × R_B)ᵧ + (r_load × F)ᵧ = 0 (r_B × R_B)ᵧ = −5Bᵤ (r_load × F)ᵧ = 250 ΣMᵧ = −5Bᵤ + 250 = 0 → Bᵤ = 50 N From Aᵤ + Bᵤ = 100: Aᵤ = 100 − 50 = 50 N Moment equations (z-axis component): ΣMᵤ = (r_B × R_B)ᵤ + (r_load × F)ᵤ = 0 (r_B × R_B)ᵤ = 0 (r_load × F)ᵤ = 432.5 ΣMᵤ = 0 + 432.5 = 0? This is inconsistent. Rethink: If there is no moment resistance at B (roller), the beam cannot be in equilibrium under this load unless there is an applied moment or the reaction at A includes a moment. A roller on a plane prevents translation but allows rotation about axes in the plane. So B can provide a reaction force normal to the plane (Bᵤ) but no moment. If the applied load creates a net moment about the z-axis, the beam cannot rotate because the roller prevents the necessary rotation. This indicates either: (a) The problem is statically indeterminate or overconstrained, or (b) An additional support or constraint is missing. For a consistent solution, assume the beam is also supported against z-rotation, perhaps by a wire preventing y-motion at B. Then Bᵧ is also a reaction. Revised: B has Bᵤ and Bᵧ (no Bₓ, assuming the z-axis is perpendicular to the plane and y is along the plane). Force equation: ΣFᵧ = Aᵧ + Bᵧ + 173.2 = 0 Moment equation about A, z-component: Bᵧ(5) − 173.2(2.5) = 0 → Bᵧ = 86.6 N Then Aᵧ = −86.6 − 173.2 = −259.8 N Moment about A, y-component: −Bᵤ(5) + (−100)(2.5) = 0 → −5Bᵤ − 250 = 0 → Bᵤ = −50 N This negative value contradicts the assumption. The problem setup may require clarification regarding the roller constraints.

Key Points

  • 3D equilibrium requires six equations: three for forces (x, y, z), three for moments (x, y, z)
  • Up to six unknowns can be solved in 3D
  • Support reactions vary: roller/surface contact (1), pin (2–3 depending on orientation), ball joint (3), fixed (6)
  • Moment is calculated as the cross product of position vector and force vector
  • Systematic component setup and careful bookkeeping are essential in 3D problems
  • Matrix methods and careful coordinate choice simplify the algebra

A structure is **statically determinate** if the number of unknown reactions equals the number of independent equilibrium equations available. For a 2D rigid body, there are three equilibrium equations, so a determinate structure has exactly three unknown reactions (or sometimes fewer if there are constraints like zero horizontal load means zero horizontal reaction). **Determinate 2D structures:** - Simply supported beam (pin + roller): 3 unknowns (Aₓ, Aᵧ, Bᵧ) ✓ - Cantilever (fixed end): 3 unknowns (Aₓ, Aᵧ, M_A) ✓ - Beam with overhang, simply supported (pin + roller, load beyond support): still 3 unknowns for the primary structure, but moments and shears vary along the span **Indeterminate structures:** - Continuous beam (more than two supports): e.g., a 10-meter beam on three supports has 4 unknown vertical reactions (minimum), exceeding the 3 equations. The structure is **statically indeterminate to the 1st degree** (4 − 3 = 1 redundant constraint). - Cantilever with additional support: e.g., a cantilever with a cable tie-down introduces extra reaction, making it overconstrained. - Two-span beam with two pins and a roller: 4 vertical reactions, indeterminate by 1. **Degree of indeterminacy:** For a 2D system: DI = (number of unknown reactions) − 3 For a 3D system: DI = (number of unknown reactions) − 6 If DI > 0, the structure is statically indeterminate. Additional equations from deformation compatibility (strain–displacement relations, material properties) are needed. These are covered in courses on **Structural Analysis** and **Mechanics of Materials** (solving via slope-deflection, moment distribution, energy methods, etc.). For the PCE exam focusing on equilibrium, you must identify when a structure is indeterminate and recognize that equilibrium equations alone are insufficient. **Practical relevance per NSCP 2015:** The NSCP 2015 (National Structural Code of the Philippines, equivalent to IBC/ACI standards) assumes structures are analyzed for their deformations and redistributions, implicitly allowing indeterminate analysis. However, mastering determinate equilibrium is the foundation. Modern design software solves indeterminate systems automatically; the engineer's role is to set up the correct model and interpret results. **Stability:** A structure must be **stable**—not in danger of infinite displacements. A beam supported at only one point (one reaction) is unstable; it rotates about that support. A 2D rigid body needs at least three reactions, and they must not be concurrent or parallel. If all three reactions are parallel (e.g., all vertical), the body is statically determinate in vertical equilibrium but unstable in horizontal equilibrium—any horizontal load causes failure.

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7. Statically Determinate vs. Indeterminate Systems

Examples

Checking Determinacy of a Beam System

Beam ABCD, 12 m total length: AB = 3 m (pin at A), BC = 6 m (roller at B), CD = 3 m (overhang). Support reactions: Aₓ, Aᵧ at pin A; Bᵧ at roller B. Three unknowns, three equations → determinate.

Worked Solution

DI = 3 − 3 = 0. The structure is determinate. Any loading can be analyzed using equilibrium equations alone. No deformation data is needed.

Indeterminate Continuous Beam

Continuous beam ABCDE, 15 m total length: Span AB = 5 m, BC = 5 m, CD = 5 m. Supports: pin at A, rollers at B, C, and D. Four vertical reactions (Aₓ = 0 if no horizontal load), Aᵧ, Bᵧ, Cᵧ, Dᵧ. With four unknowns and three equations, the structure is indeterminate.

Worked Solution

Unknown reactions: Aᵧ, Bᵧ, Cᵧ, Dᵧ (horizontal reaction Aₓ = 0 due to symmetry or no horizontal load). DI = 4 − 3 = 1. The structure is indeterminate to the first degree. Solving requires compatibility of deformation (slopes and deflections at supports are zero); methods include slope-deflection, moment distribution, or matrix stiffness. Equilibrium alone cannot determine the reactions uniquely.

Key Points

  • A determinate 2D structure has exactly 3 unknown reactions for 3 equilibrium equations
  • Indeterminate structures have more unknowns than equations; additional information (deformation) is needed
  • Degree of indeterminacy: DI = (unknowns) − (equations); positive DI means indeterminate
  • Stability requires at least 3 non-concurrent, non-parallel reactions in 2D
  • Supports must prevent all possible rigid-body motions (translation and rotation)
  • PCE focus: Identify determinate vs. indeterminate; apply equilibrium to determinate problems only

**Couples and Moments:** A **couple** is a pair of equal, opposite, parallel forces separated by a distance. The moment of a couple is M = F × d (force × perpendicular distance), and it is independent of the moment point—the same for all points. Couples are often applied as concentrated moments in problems (e.g., torque from a motor, bending moment applied externally). **Principle of Superposition:** For linear systems (which most equilibrium problems are), the effect of multiple loads is the sum of the effects of each load individually. You can solve each load separately and add the reactions. This is useful for complex loading patterns or checking solutions. **Zero-Force Members in Trusses:** In a truss, a member carries zero force if (1) at a joint, the member is collinear with another member and there is no external load at the joint, or (2) two non-collinear members meet at a joint with no external load. These members can sometimes be omitted from the analysis or design, though they may be kept for stability or to prevent local buckling. **Mechanical Efficiency and Inclined Supports:** When an inclined support is present (e.g., a beam resting on a 30° slope), the reaction is perpendicular to the slope. The angle of the reaction is fixed by geometry, not by the force balance. This constrains the problem; only one unknown (magnitude) remains for that support, not two. **Distributed Moments:** Some problems involve distributed moments (moment per unit length, analogous to distributed load). The resultant is the integral of the moment distribution. Fortunately, these are rare in introductory equilibrium; they appear more in advanced courses. **Friction and Rough Surfaces:** If a support is "rough" (friction is present), the reaction has both normal and tangential (frictional) components. The magnitude of friction is limited by f ≤ μN, where μ is the coefficient of friction and N is the normal force. Problem statements must specify whether surfaces are "smooth" (frictionless) or rough and provide μ if needed. **Partial Supports and Yielding:** In rare cases, a support may fail or yield (e.g., a cracked foundation, a cable over its breaking strength). If the problem states a support fails, remove it from the FBD and solve the reduced system. If a cable has a maximum tension, check if the equilibrium solution exceeds it; if so, the cable fails, and the problem is no longer solvable with that cable in place—a dynamic or dynamic response analysis is needed.

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8. Special Cases and Advanced Concepts

Examples

Couple Applied to a Beam

A simply supported beam AB (6 m) carries a point load of 60 kN at 2 m from A and a concentrated moment (couple) of 40 kN·m applied at 4 m from A (clockwise as viewed from above). Find the reactions.

Worked Solution

FBD: Aₓ (= 0), Aᵧ, Bᵧ, point load 60 kN downward at 2 m, and moment 40 kN·m clockwise. ΣM_A = 0 (taking counterclockwise as positive): Bᵧ(6) − 60(2) − 40 = 0 (the couple contributes −40, assuming clockwise is negative) 6Bᵧ = 120 + 40 = 160 Bᵧ = 26.67 kN ΣF_y = 0: Aᵧ + Bᵧ − 60 = 0 Aᵧ = 60 − 26.67 = 33.33 kN Note: The couple does not appear in the force equation (ΣF_y), only in the moment equation. This is a key property of couples.

Beam on Inclined Support

A beam AB (4 m) has a pin at A (horizontal surface) and a roller on a 30° slope at B. A vertical load of 100 kN acts at the center (2 m from A). Find the reactions.

Worked Solution

At A (pin): Aₓ, Aᵧ (both unknown, two unknowns). At B (roller on 30° slope): One reaction perpendicular to the slope, magnitude R_B (one unknown). The reaction at B has components: R_{Bx} = R_B sin(30°) = 0.5 R_B (pointing down-left along the slope), R_{By} = R_B cos(30°) = 0.866 R_B (pointing up-left perpendicular to the slope). Total unknowns: 3 (Aₓ, Aᵧ, R_B). Three equations available. Determinate. ΣF_y = 0: Aᵧ + R_B cos(30°) − 100 = 0 Aᵧ + 0.866 R_B = 100 ... (1) ΣF_x = 0: Aₓ − R_B sin(30°) = 0 Aₓ = 0.5 R_B ... (2) ΣM_A = 0: R_B cos(30°) × 4 − 100 × 2 = 0 3.464 R_B = 200 R_B = 57.74 kN From (1): Aᵧ = 100 − 0.866(57.74) = 100 − 50 = 50 kN From (2): Aₓ = 0.5(57.74) = 28.87 kN Interpretation: The pin provides reactions of 28.87 kN horizontal and 50 kN vertical. The inclined support provides 57.74 kN perpendicular to its surface.

Key Points

  • A couple is a pair of equal, opposite forces; its moment is the same at all points (independent of moment point)
  • Superposition: total effect of multiple loads is the sum of individual effects (for linear systems)
  • Zero-force members in trusses can sometimes be identified by inspection and omitted
  • Inclined supports constrain the reaction direction; only magnitude is unknown for that support
  • Friction on rough surfaces adds a tangential component limited by f ≤ μN
  • If a support fails, remove it and resolve; check cable/support capacities against calculated tensions
  • Distributed moments are rare in basic equilibrium but require integration to find their resultant

**Mistake 1: Wrong Support Reactions** Many students confuse the reactions provided by different supports: - A **roller** provides only **one normal reaction** (perpendicular to the surface); it cannot resist shear along the surface or moment. - A **pin (hinge)** provides **two reactions** (horizontal and vertical, or any two orthogonal directions). It cannot resist moment about the hinge axis. - A **fixed end** provides **three reactions**: two forces and one moment. It can resist all three. **Solution:** Sketch the support symbol and ask: "Can this support move in this direction?" If yes, there is no reaction in that direction. If no, there is. **Mistake 2: Taking Moments About the Wrong Point** Students often take moments about a random point, leading to algebra with multiple unknowns. The strategic choice is to take moments about a support point, eliminating its reaction from the equation. **Solution:** Identify which reaction you want to eliminate or which one is already known, and take moments about the point where that reaction acts. For a simply supported beam, take moments about one support to find the reaction at the other support; then use force balance. **Mistake 3: Forgetting Distributed Loads or Misplacing the Resultant** A uniformly distributed load (UDL) must be converted to a resultant force. The magnitude is q × L (intensity × length), but the position is critical—it acts at the **centroid** of the load region, not at a random point. - **Uniform load over length L:** Resultant at L/2 from either end. - **Triangular load (full height at one end, zero at the other):** Resultant at L/3 from the zero end, 2L/3 from the full-height end. - **Trapezoidal load:** Must compute the centroid by geometry or integration. **Solution:** Sketch the distributed load and its resultant. Use the geometry of the load shape to find the centroid, or use integration: centroid position x̄ = ∫ x q(x) dx / ∫ q(x) dx. **Mistake 4: Lami's Angle Errors** Lami's Theorem is powerful, but the angle definition is often misunderstood. Each angle α_i is the angle **between the other two forces**, not the angle from a reference axis. **Solution:** Sketch the three forces as vectors emanating from a point. At each force, the angle is at that vertex between the other two forces. Use a protractor or geometry to measure; do not assume angles from the problem statement apply directly to Lami. **Mistake 5: Sign Convention Confusion** When solving equilibrium equations, we choose a positive direction (e.g., rightward, upward, counterclockwise). If a calculated reaction is negative, it means the reaction is opposite to the assumed direction. Many students treat negative results as errors, but they are not—they are correct interpretations of the directions. **Solution:** State the sign convention clearly at the start. When the answer is negative, state it as "R = −X kN, indicating a [opposite direction]." Verify using a check equation (e.g., moment sum about a different point). **Mistake 6: Ignoring Horizontal Components** Problems with inclined loads often have horizontal components that must be included in ΣFₓ = 0. Forgetting these leads to unbalanced horizontal forces. **Solution:** Always apply all three equilibrium equations: ΣFₓ = 0, ΣFᵧ = 0, ΣM = 0. Inclined load components must be decomposed: Fₓ = F cos(θ), Fᵧ = F sin(θ). **Mistake 7: Confusing Particles and Rigid Bodies** Particles have concurrent forces only (forces meet at a point); rigid bodies can have non-concurrent forces. For particles, only two equations (ΣFₓ = 0, ΣFᵧ = 0) are needed. For rigid bodies, three are needed (ΣFₓ = 0, ΣFᵧ = 0, ΣM = 0). **Solution:** Read the problem carefully. If all forces are applied at one point, treat it as a particle. If forces are applied at different points (loads at different locations along a beam), treat it as a rigid body and include the moment equation.

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9. Common Board Exam Mistakes and Solutions

Examples

Mistake: Wrong Support Type Leads to Wrong Unknowns

A student mistakenly treats a roller support as a pin, assuming it provides both normal and tangential (horizontal) reactions. The problem asks for three unknowns: Aₓ, Aᵧ, and Bᵧ, but the student sets up Aₓ, Aᵧ, Bₓ, Bᵧ (four unknowns for three equations). The system becomes unsolvable.

Worked Solution

Correct approach: Identify the support type correctly. A roller on a level surface provides Bᵧ only (perpendicular to the surface). No Bₓ. This reduces unknowns to Aₓ, Aᵧ, Bᵧ—three for three equations. The system is determinate. If there is no horizontal applied force, ΣFₓ = 0 yields Aₓ = 0 directly, simplifying further.

Mistake: Distributed Load Resultant at Wrong Location

A beam carries a UDL of 20 kN/m over a 4 m span from x = 2 m to x = 6 m. A student places the 80 kN resultant at x = 4 m (midpoint of the span 2 to 6) but should place it at x = 4 m, which is correct. But another student places it at x = 3 m (distance 1 m from the left edge of the load), a common error.

Worked Solution

Correct calculation: Load region from x = 2 to x = 6 is a 4 m span. Centroid at x = 2 + 4/2 = 4 m. Resultant = 20 × 4 = 80 kN at x = 4 m. Taking moments about x = 0, the moment is 80 × 4 = 320 kN·m, not 80 × 3 = 240 kN·m (if placed at x = 3). The error propagates through the entire solution.

Key Points

  • Roller = 1 reaction; Pin = 2 reactions; Fixed = 3 reactions
  • Take moments about a support to eliminate that support's reaction from the equation—saves algebra
  • Distributed loads must be converted to resultants at the centroid, not at arbitrary points
  • Lami angles are between the other two forces, not from a reference axis—sketch to avoid errors
  • Negative results are correct; they indicate the reaction is opposite to the assumed direction
  • Always include horizontal equilibrium (ΣFₓ = 0), not just vertical (ΣFᵧ = 0)
  • Particles need two equations (forces only); rigid bodies need three (forces + moments)
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