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CELE Engineering MechanicsFrames, Machines and CablesDetailed Explanation

The Frames, Machines and Cables chapter rewards slow, careful thinking over quick pattern matching, especially on Professional Regulation Commission (PRC) — Board of Civil Engineering's scenario-based CELE items. This detailed explanation walks through the full derivation of every core idea, then links each one to a worked example pulled from recent CELE Engineering Mechanics papers.

Exam context

Professional Regulation Commission (PRC) — Board of Civil Engineering runs the Civil Engineer Licensure Examination on May and November 2026. Its Engineering Mechanics section sits under a "Core" weighting, and Frames, Machines and Cables is the 4th chapter in the 8-chapter CELE Engineering Mechanics rotation. The CELE passing mark is 70% weighted average, no sub-test below 50%, and the most recent 2026 paper drew about a meaningful share of questions from Engineering Mechanics.

Frames, Machines and Cables - Detailed Explanation

Frames, machines, and cables represent three fundamental structural systems that every civil engineer must analyze with confidence. Unlike trusses — where every member is a two-force member carrying only axial load — frames and machines contain at least one multi-force member that develops shear and bending in addition to axial force. Cables, on the other hand, are the purest tension-only structures, taking a geometry entirely dictated by the applied loading. These three topics appear regularly in the PRC Civil Engineer Licensure Examination (CE Board Exam) and demand a systematic approach: correct free-body diagrams (FBDs), disciplined application of the three equilibrium equations, and the ability to recognize special members that simplify the solution. This chapter provides a comprehensive, board-exam-focused treatment of all three systems, complete with worked examples in SI units, common pitfalls, and exam strategies.

Concepts

Frames — Definition, Classification, and Analysis Strategy

A frame is a stationary structure designed to support loads. What distinguishes it from a truss is the presence of at least one multi-force member — a member that is (a) connected to more than two points, (b) subjected to a transverse load along its length, or (c) carries a couple/moment. Because of these multi-force members, internal forces are not purely axial; shear and bending are present. The standard analysis procedure has three distinct phases: PHASE 1 — IDENTIFY TWO-FORCE MEMBERS. Before drawing any FBD, inspect every member. A two-force member is connected at exactly two points, has no loads applied between those points, and carries no couple. Its resultant force must act along the line connecting its two pin joints. Identifying these members first eliminates unknowns and dramatically simplifies the solution. PHASE 2 — EXTERNAL REACTIONS. Treat the entire frame as a single rigid body and apply the three equilibrium equations (ΣFx = 0, ΣFy = 0, ΣM = 0) to find the support reactions. This step is independent of the internal pin forces and provides the boundary conditions for the next phase. PHASE 3 — DISMEMBER AND APPLY EQUILIBRIUM. Separate the frame at every pin joint. On each member's FBD, the pin force has two unknown components (Cx, Cy for a pin at C). By Newton's Third Law, if pin C pushes member AB in the +x direction, it pushes member CD in the −x direction — these forces are equal in magnitude, opposite in direction. Write ΣFx = 0, ΣFy = 0, ΣM = 0 for each member. Choose moments about a pin that carries two unknowns — this often allows solving for one unknown directly. A frame is statically determinate if the total number of unknowns equals the total number of available equilibrium equations. For a frame with m members and r reaction components, determinacy requires m × 3 equations ≥ unknowns. In practice, most CE Board exam frames are explicitly statically determinate.

Examples

The key insight is recognizing strut CD as a two-force member, which tells us immediately that its force acts at 45°. This reduces the unknowns on the beam FBD from four to three (Ax, Ay, FCD), solvable with three equations. Taking moments about A eliminates both pin components at A, giving FCD in one equation.

Scenario

Beam AB (horizontal, 6 m long) is pinned to a wall at A(0,0) and propped at its midpoint C(3,0) by a strut CD running to D(0,−3). A vertical load of 12 kN acts at the free end B(6,0). Find the strut force and the pin reaction at A.

Solution

Step 1 — Identify two-force member: Strut CD is loaded only at C and D (two pins, no loads along its length) → two-force member. The strut runs from D(0,−3) to C(3,0), so its direction angle θ = arctan(3/3) = 45° from horizontal. The force in CD acts along this 45° line. Step 2 — FBD of beam AB. Forces acting on beam AB: • At A: Ax (→) and Ay (↑) — unknown pin components • At C: Strut pushes beam at 45° — components FCD·cos45° (→) and FCD·sin45° (↑) • At B: 12 kN (↓) applied load Step 3 — Take moments about A (eliminates Ax and Ay): ΣMA = 0: (FCD·sin45°)(3) − 12(6) = 0 FCD·sin45° = 72/3 = 24 kN FCD = 24/sin45° = 24/0.7071 = 33.94 kN (compression in strut) Step 4 — Solve for Ay: ΣFy = 0: Ay + FCD·sin45° − 12 = 0 Ay = 12 − 24 = −12 kN → 12 kN downward Step 5 — Solve for Ax: ΣFx = 0: Ax + FCD·cos45° = 0 Ax = −24 kN → 24 kN toward wall (leftward) Step 6 — Resultant at A: RA = √(24² + 12²) = √(576 + 144) = √720 = 26.8 kN Answer: Strut force FCD = 33.9 kN (compression); Pin reaction at A = 26.8 kN

For a two-force member, the pin force magnitude equals the member force. The resultant at pin E equals F_CE. This is a standard board-exam configuration — always check for the two-force simplification before writing equations.

Scenario

A frame consists of a vertical post CE (pinned at C to the floor, pinned at E to a horizontal beam), and a horizontal beam AE (pinned to wall at A, free end at B). A 20 kN vertical load is at midspan of AE. CE is a two-force member inclined at 30° to the vertical. Span AE = 4 m, load at 2 m from A. Find pin force at E.

Solution

Step 1: CE is a two-force member at 30° from vertical (60° from horizontal). Let F_CE = force in CE. Step 2: FBD of beam AE: • At A: Ax, Ay (wall pin) • At E: F_CE acts along CE direction — components F_CE·sin30° (horizontal, pushing beam rightward if CE is in compression) and F_CE·cos30° (vertical, pushing beam upward) • 20 kN downward at 2 m from A Step 3: ΣMA = 0 (on beam AE, moment about A): (F_CE·cos30°)(4) − 20(2) = 0 F_CE = 40/(4 × 0.866) = 40/3.464 = 11.55 kN Step 4: Pin force at E on beam = F_CE = 11.55 kN at 30° from vertical Components: Ex = 11.55·sin30° = 5.77 kN; Ey = 11.55·cos30° = 10.0 kN Resultant: √(5.77² + 10²) = 11.55 kN (as expected for a two-force member)

Applications

  • Structural analysis of roof trusses with knee braces (the knee brace is typically a two-force member).
  • Analysis of crane booms, derricks, and loading frames — multi-force members under combined axial and transverse loads.
  • Bracket connections on building facades where the bracket plate is a multi-force member.
  • Analysis of formwork falsework frames per NSCP 2015 provisions on construction loads.
  • Portal frame structures — a staple of Philippine low-rise industrial buildings analyzed as frames with rigid joints.

Misconceptions

  • WRONG: 'The diagonal brace in a frame is always a two-force member.' — CORRECT: Only if it has exactly two pin connections and zero intermediate loads. A diagonal with a load at its midpoint is a multi-force member.
  • WRONG: 'Pin forces on connected members point in the same direction.' — CORRECT: Newton's 3rd Law — equal in magnitude, OPPOSITE in direction.
  • WRONG: 'I can skip Phase 2 (whole-body reactions) and just dismember.' — CORRECT: Whole-body reactions provide essential boundary conditions. Without them, you have too many unknowns.
  • WRONG: 'A frame is only statically determinate if it looks symmetric.' — CORRECT: Determinacy depends on the equation count vs. unknown count, not geometry or symmetry.
  • WRONG: 'The pin force at a joint equals the sum of the forces on both members.' — CORRECT: The pin force on each member equals the force that pin exerts on that member; equal and opposite forces on each side.

Related Concepts

  • Truss analysis (method of joints, method of sections) — trusses are a special case with all two-force members
  • Static equilibrium — ΣFx=0, ΣFy=0, ΣM=0
  • Newton's Third Law applied at internal pins
  • Free body diagrams (FBD) construction
  • Moment of a force about a point

Common Exam Questions

Example

Frame with members AC and BC, pinned at A (wall), B (wall), and C (shared). Load P at C. Find forces at A and B. → Identify whether AC or BC is a two-force member, then take moments on the multi-force member.

Approach

Draw FBD of each member, apply Newton's 3rd Law at shared pins. Take moments about a pin to eliminate unknowns.

Question Type

Find pin force at a joint after dismembering

Example

Given a frame with members described by geometry and loading, the board exam asks: 'Which member is a two-force member?' → Member with two pin connections and no intermediate loads.

Approach

Check: (1) exactly two pin connections, (2) no loads between pins, (3) no couples. If all three — two-force member.

Question Type

Identify two-force vs multi-force members

Example

L-shaped frame pinned at A, roller at D, loaded at B. Find RD. → Use whole-body ΣMA = 0 first, then dismember if pin forces are also asked.

Approach

Step 1: whole-body FBD for reactions. Step 2: dismember, write equations for each member.

Question Type

Find support reactions of a frame then internal pin force

Key Points To Remember

  • A frame has at least one multi-force member — if all members are two-force, it is a truss.
  • Always identify two-force members first — their force direction is known (along the member axis), eliminating unknowns.
  • Phase 1: External reactions on the whole frame. Phase 2: Dismember, apply Newton's 3rd Law at pins.
  • At each shared pin, forces on the two connected members are equal in magnitude and opposite in direction.
  • Choose the moment center at a point where the most unknowns have zero moment arm — usually a pin with two unknowns.
  • A frame is stationary (not moving); a machine has moving parts. Both use the same analysis method.
  • Internal pin forces are NOT reactions — they are internal to the structure but external to each individual member FBD.

Machines — Mechanical Advantage and Force Transmission

A machine is structurally identical to a frame in its analysis method — it contains multi-force members and is analyzed by dismembering and applying equilibrium. The critical difference is purpose and motion: machines are designed to transmit or transform forces, and their parts can move relative to each other. The fundamental quantity for a machine is its MECHANICAL ADVANTAGE (M.A.): M.A. = Output force (load) / Input force (effort) For a simple lever (the most common machine on the CE Board Exam): • M.A. = effort arm / load arm • This follows directly from ΣM = 0 about the fulcrum: F_effort × d_effort = F_load × d_load For compound machines (machines in series), the overall M.A. is the product of the individual M.A.s. In the CE Board Exam, machine problems typically present pliers, bolt cutters, can openers, toggle clamps, or scissors. The procedure is always the same: 1. Identify the input pin (where effort is applied) and output pin (where load is delivered). 2. Draw FBD of each rigid part — the pivot pin forces are internal. 3. Apply ΣM = 0 about the pivot to relate effort to load. For a TOGGLE CLAMP (common in board exams): the mechanical advantage becomes very large as the toggle angle approaches 0° (links become nearly horizontal) — theoretically infinite at θ = 0. This is why toggle clamps are used in jigs and fixtures: a moderate effort produces a very large clamping force. For PULLEY SYSTEMS: M.A. equals the number of rope segments supporting the load (for an ideal, frictionless pulley). A movable pulley system with n supporting ropes has M.A. = n.

Examples

The lever multiplies force by a factor of 8 — for every 1 N of effort, 8 N of load is balanced. This is the classic board-exam lever problem. Note that if the load arm were equal to the effort arm, M.A. = 1 (no mechanical advantage, just force redirection).

Scenario

A lever (Class 1) has a fulcrum dividing it such that the effort arm is 400 mm and the load arm is 50 mm. An effort of 50 N is applied. Find: (a) the load the lever can balance, and (b) the mechanical advantage.

Solution

Step 1 — Apply ΣM = 0 about fulcrum: F_effort × d_effort = F_load × d_load 50 N × 400 mm = F_load × 50 mm F_load = 50 × 400/50 = 400 N Step 2 — Mechanical Advantage: M.A. = F_load / F_effort = 400/50 = 8 Alternately: M.A. = d_effort/d_load = 400/50 = 8 ✓ Answer: Load = 400 N; M.A. = 8

The pliers acts as a force amplifier. In a real pliers problem, the board exam may give you the complete geometry (distances on the handle and jaw sides) and ask for the jaw force on a bolt or wire being cut. Always take moments about the pivot pin — the pivot reaction drops out.

Scenario

A pair of pliers has its pivot pin at 20 mm from the jaw tips and at 80 mm from where the hand grips. A 60 N hand force is applied at the grip. What gripping force do the jaws exert?

Solution

Step 1 — Identify: This is a Class 1 lever. Pivot is between effort and load. Effort arm = 80 mm (from pivot to hand grip) Load arm = 20 mm (from pivot to jaw tip) Step 2 — ΣM = 0 about pivot pin: 60 N × 80 mm = F_jaw × 20 mm F_jaw = 60 × 80/20 = 240 N Answer: Jaw gripping force = 240 N (M.A. = 4)

Each rope segment in an ideal pulley carries the same tension (equal to effort). Three segments → three times the effort supports the load. This is a common mechanical engineering/physics concept that also appears in CE Board mechanics problems.

Scenario

An ideal movable pulley system uses 3 rope segments to support a load. If the effort is 200 N, what is the maximum load that can be lifted?

Solution

For an ideal pulley system with n rope segments supporting the load: M.A. = n = 3 Load = M.A. × Effort = 3 × 200 = 600 N Answer: Maximum load = 600 N

Applications

  • Construction equipment: hydraulic jacks, manual hoists, chain blocks — all machines analyzed by equilibrium and M.A.
  • Scaffolding clamps and formwork tightening devices — toggle-action clamps provide high clamping force from modest hand effort.
  • Rebar benders and cutters on Philippine construction sites — lever machines with defined M.A.
  • Crane hook blocks with multiple sheave pulleys — pulley system M.A. calculation is used in rigging design.
  • Traffic barrier deployment arms — linkage mechanisms analyzed as machines.

Misconceptions

  • WRONG: 'A machine with M.A. > 1 gives free energy.' — CORRECT: Work input = Work output (ideal). Higher force means smaller displacement: W = F × d is conserved.
  • WRONG: 'The pivot force in a lever is zero.' — CORRECT: The pivot reaction equals the sum of all other forces on the lever; take ΣF = 0 to find it.
  • WRONG: 'Pulley M.A. always equals the number of pulleys.' — CORRECT: M.A. = number of rope segments supporting the load, not number of pulleys.
  • WRONG: 'A machine analysis requires dynamics because parts move.' — CORRECT: In CE Board problems, machines are analyzed in STATIC equilibrium at any given position — forces are balanced, no acceleration.

Related Concepts

  • Simple lever classes (Class 1, 2, 3)
  • Virtual work principle — alternative method for machines
  • Friction in machines — efficiency η = M.A._actual / M.A._ideal
  • Hydraulic press — Pascal's Law as a fluid 'machine'
  • Pulley systems and mechanical advantage

Common Exam Questions

Example

A bolt cutter has handles 300 mm long and jaw opening 30 mm from pivot. A 150 N force on each handle — what force on the bolt? → F_bolt = 150 × (300/30) = 1500 N

Approach

Apply ΣM = 0 about the pivot. Output force = effort × (effort arm / load arm).

Question Type

Find the output force given effort and M.A.

Example

A wheelbarrow: load at 0.3 m from wheel axle, effort (lift) at 1.5 m from axle. M.A. = 1.5/0.3 = 5.

Approach

M.A. = effort arm / load arm. Locate the fulcrum/pivot, measure both arms.

Question Type

Find mechanical advantage of a given machine geometry

Example

Hydraulic shear: Find the force in the hydraulic ram given the cutting force and geometry — take moments about the frame pivot.

Approach

Dismember the machine, apply ΣF and ΣM to each part.

Question Type

Machine equilibrium — find pin/pivot reactions

Key Points To Remember

  • Machines have moving parts; frames are stationary. Same analysis method applies to both.
  • M.A. = load/effort = effort arm/load arm (for a lever, from ΣM = 0 about fulcrum).
  • An ideal machine has 100% efficiency: effort × effort arm = load × load arm.
  • Real machines have M.A. < theoretical due to friction — but CE Board problems usually assume frictionless (ideal).
  • For toggle mechanisms, M.A. → ∞ as toggle angle → 0° — the toggle is at dead center.
  • Identify the pivot/fulcrum first — this is the moment center that decouples effort from load.
  • Compound machine M.A. = product of individual M.A. values.

Cables Under Concentrated Loads

A cable is a perfectly flexible, inextensible member that can carry only tension — no compression, no shear, no bending. Because it has no bending stiffness, a cable cannot be 'bent' by a couple; it simply adjusts its geometry. This means the cable's shape is determined by the loads applied to it. KEY PRINCIPLE — CONSTANT HORIZONTAL COMPONENT: For any cable under vertical loads only (no horizontal distributed load), the horizontal component of tension H is the same at every point along the cable. This is proven by isolating any segment of the cable: ΣFx = 0 for the segment forces left and right means Hleft = Hright = H = constant. At any point where the cable makes angle θ with the horizontal: T = H / cos θ or equivalently: H = T cos θ The tension T varies along the cable, reaching its maximum at the steepest point — at the supports if the supports are at the same elevation. ANALYSIS OF CABLE WITH CONCENTRATED LOADS: 1. Draw the FBD of the entire cable. The loads are known; the support reactions have both horizontal and vertical components (roller supports would be impractical for a cable — both supports are pins). 2. Apply ΣM = 0 about one support to find the vertical reaction at the other support. 3. Find the vertical reaction at the first support from ΣFy = 0. 4. The horizontal reactions at both supports are equal and opposite: both equal H. 5. Find H by taking ΣM = 0 about any load point, using the known geometry (sag at that point). 6. Compute tension in each segment: T = H / cos θ_segment. For a cable with a single central load at midspan with sag d and half-span L/2: tan θ = d / (L/2) = 2d/L T = H / cos θ, and from ΣFy at the load point: 2T sin θ = P → T = P/(2 sin θ)

Examples

For a symmetric central load, both halves of the cable are mirror images. The horizontal component H = 20 kN is constant in both halves (as expected). The cable tension T = 20.6 kN > H because the cable is inclined, not horizontal.

Scenario

A cable of span 12 m carries a single 10 kN vertical load at midspan. The sag at the load is 1.5 m. Find the cable tension and the horizontal component H.

Solution

Step 1 — Geometry: The cable is symmetric. Each half makes angle θ with horizontal. tan θ = sag / half-span = 1.5 / 6.0 = 0.25 θ = arctan(0.25) = 14.04° sin θ = 0.2425, cos θ = 0.9701 Step 2 — Equilibrium at load point (ΣFy = 0): Vertical components of both cable segments must balance the 10 kN load: 2T sin θ = 10 kN T = 10 / (2 × 0.2425) = 10 / 0.485 = 20.62 kN Step 3 — Horizontal component: H = T cos θ = 20.62 × 0.9701 = 20.0 kN Answer: Cable tension T = 20.6 kN; Horizontal component H = 20.0 kN Note: By symmetry, both cable segments have the same tension since both make the same angle.

The middle segment BC is horizontal because of symmetric loading at symmetric points — this is a common board-exam configuration. The horizontal tension equals H exactly when the segment is flat. Maximum tension is at the steepest segments AB and CD, at the supports.

Scenario

A cable spans 9 m and carries two equal 8 kN loads at the third points (3 m and 6 m from the left support). The sag at the left load point is 2 m. Find H and the tension in each segment.

Solution

Step 1 — Label points: Left support A(0,0), load point B(3,−2), load point C(6, y_C), right support D(9,0). Step 2 — By symmetry of equal loads at equal spacings: The cable is symmetric. y_C = −2 m also. Step 3 — FBD of entire cable: Supports at A and D. Two 8 kN loads at B and C. From symmetry: Ay = Dy = (8+8)/2 = 8 kN (↑) Horizontal: Ax = H → (to the right), Dx = H → (to the left) Step 4 — Find H using the geometry of segment AB: Slope of AB: from A(0,0) to B(3,−2): tan θ_AB = 2/3 → θ_AB = 33.69° The vertical reaction at A supports segment AB vertically: Ay = H tan θ_AB 8 = H × (2/3) H = 8 × 3/2 = 12 kN Step 5 — Check with segment BC: B(3,−2) to C(6,−2): horizontal segment → θ_BC = 0° T_BC = H / cos 0° = 12 / 1 = 12 kN (horizontal tension in middle segment) Step 6 — Tension in segment AB (and by symmetry, CD): θ_AB = arctan(2/3) = 33.69°; sin θ = 0.5547; cos θ = 0.8321 T_AB = H / cos θ_AB = 12 / 0.8321 = 14.42 kN Answer: H = 12 kN; T_AB = T_CD = 14.4 kN; T_BC = 12.0 kN (horizontal middle segment)

Applications

  • Suspension bridges (e.g., conceptual analysis of the Pasig River cable-stayed/suspension schemes)
  • Cable-supported roofs — convention centers, sports arenas
  • Power transmission lines — sag calculation for clearance to ground (PEC requirements)
  • Aerial tramways and ski lift cables — segment-by-segment tension analysis
  • Overhead cranes with hanging cables — maximum sag check under load

Misconceptions

  • WRONG: 'The cable tension is the same everywhere.' — CORRECT: Only the HORIZONTAL COMPONENT H is constant. The total tension T = H/cos θ varies with the slope.
  • WRONG: 'Maximum cable tension is at midspan.' — CORRECT: Maximum is at the steepest point — at the supports (for cables with supports at same or different elevations, it's at the higher/steeper end).
  • WRONG: 'A slack cable can carry compression under load.' — CORRECT: A cable can NEVER carry compression — it simply goes slack (loses tension and changes shape).
  • WRONG: 'Cable geometry can be chosen freely.' — CORRECT: Under a given set of loads, there is only one equilibrium shape for a given H. The shape is determined by the loads and H.
  • WRONG: 'For two equal symmetric loads at third-points, all segments have the same tension.' — CORRECT: The middle horizontal segment has T = H; the outer inclined segments have T = H/cos θ > H.

Related Concepts

  • Funicular polygon (string polygon) — graphical method for cable shape
  • Trusses — comparison of pure tension (cables) vs axial-only members
  • Resultant of concurrent forces — cable equilibrium at each load point
  • Vector resolution of forces
  • Three-force body equilibrium

Common Exam Questions

Example

Cable carries 15 kN at midspan, span = 10 m, sag = 2 m. Find T. → tan θ = 2/5 = 0.4, θ = 21.8°, sin θ = 0.371, T = 15/(2×0.371) = 20.2 kN

Approach

Compute angle θ from sag geometry. Use T = H/cos θ or 2T sin θ = P at load point.

Question Type

Find tension in a cable segment given sag and load

Example

Cable with two loads — find H. Take ΣM about one support to find vertical reactions, then use the geometry at a known sag point to extract H.

Approach

H is constant. Use vertical equilibrium at any load point: ΣFy = 0 → T sin θ components balance load. H = T cos θ.

Question Type

Find horizontal tension H given cable geometry

Example

Given multiple loads, which segment has max tension? → The segment with largest inclination angle θ.

Approach

Maximum tension is at the steepest segment. For cables with supports at the same elevation, max T is at the end segments (at the supports).

Question Type

Where is the maximum tension in the cable?

Key Points To Remember

  • A cable carries tension ONLY — no compression, shear, or bending.
  • The horizontal component of tension H is CONSTANT throughout the cable (for vertical loads).
  • Maximum tension occurs at the steepest segment — at the highest support.
  • Cable geometry is determined by loads, not by the cable itself (no bending stiffness).
  • For a single concentrated load at midspan: T = P / (2 sin θ), where θ = arctan(2d/L).
  • For multiple loads: use funicular polygon — cable is straight between loads.
  • Always find H first (using moment equation about a load point), then compute tensions.

Cables Under Distributed Loads — Parabolic and Catenary Cables

When the load is distributed continuously rather than concentrated at points, the cable takes a curved shape. The two most important cases for the CE Board Exam are: ━━━━━━━━━━━━━━━━━━━━━━ 1. PARABOLIC CABLE — Load Uniform Per Unit HORIZONTAL Length (w in N/m) ━━━━━━━━━━━━━━━━━━━━━━ This is the case for a suspension bridge deck: the deck load (dead load + live load) is uniform per horizontal distance. The cable takes the shape of a PARABOLA. Key formulas for a parabolic cable with span L and midspan sag d: Horizontal tension at crown (minimum tension): H = wL² / (8d) Vertical reaction at each support (symmetric case): V = wL / 2 Maximum tension (at supports, steepest point): T_max = √(H² + V²) = √[H² + (wL/2)²] Cable length (approximate, for d/L < 1/10): S ≈ L[1 + (8/3)(d/L)²] Note: The equation of the parabola with origin at the crown (lowest point) is: y = (w/2H)x² = (4d/L²)x² ━━━━━━━━━━━━━━━━━━━━━━ 2. CATENARY CABLE — Load Uniform Per Unit CABLE LENGTH (w in N/m of cable) ━━━━━━━━━━━━━━━━━━━━━━ This is the shape taken by a cable under its own self-weight (uniform weight per unit cable length). The curve is a CATENARY, defined by the hyperbolic cosine function: y = (H/w)·cosh(wx/H) − H/w The parameter c = H/w is the catenary constant. For most CE Board problems involving self-weight, the sag-to-span ratio is small (d/L < 0.1), making the parabola an excellent approximation of the catenary. In such cases, use the parabolic formulas with w = weight per unit length of cable. ━━━━━━━━━━━━━━━━━━━━━━ KEY DISTINCTION — PARABOLA vs CATENARY: ━━━━━━━━━━━━━━━━━━━━━━ • Load uniform per HORIZONTAL distance → PARABOLA (suspension bridge deck) • Load uniform per CABLE LENGTH → CATENARY (hanging chain, power line under self-weight) • For small sag (shallow cable): Parabola ≈ Catenary — use parabolic formulas for both. For the CE Board Exam: If the problem says 'uniform load along the horizontal' or 'uniformly distributed load on the span' → use parabolic formula. If it says 'uniform load along the cable' or 'cable weight per meter of cable' → use catenary (or parabola approximation for small sag).

Examples

This is a classic board-exam suspension bridge cable problem. The horizontal component H = 300 kN is constant throughout the cable. The maximum tension T_max = 323 kN occurs at the supports where the cable is steepest. Note: d/L = 4/40 = 0.10 — this is at the boundary where the parabolic approximation is still valid.

Scenario

A suspension cable spans 40 m horizontally with a sag of 4 m. The cable supports a uniformly distributed deck load of 6 kN/m of horizontal span. Find: (a) H, (b) T_max, (c) vertical reactions at the supports.

Solution

Given: L = 40 m, d = 4 m, w = 6 kN/m Step 1 — Horizontal tension at crown: H = wL² / (8d) = 6 × (40)² / (8 × 4) = 6 × 1600 / 32 = 9600/32 = 300 kN Step 2 — Vertical reaction at each support (symmetric cable): V = wL/2 = 6 × 40/2 = 120 kN Step 3 — Maximum tension (at supports): T_max = √(H² + V²) = √(300² + 120²) = √(90000 + 14400) = √104400 = 323.1 kN Step 4 — Angle at support: θ = arctan(V/H) = arctan(120/300) = arctan(0.4) = 21.80° Answer: H = 300 kN; T_max = 323 kN; V = 120 kN each support

The sag-to-span ratio of 0.05 justifies the parabolic approximation for this catenary problem. In the CE Board Exam, when d/L < 0.10, use the parabolic formulas regardless of whether the load is described as 'per meter of cable' — the error is less than 1%.

Scenario

A cable weighing 0.5 kN/m of its own length is strung between two towers 100 m apart at the same elevation. The sag at midspan is 5 m. Determine the maximum tension in the cable. (Use parabolic approximation.)

Solution

Given: w = 0.5 kN/m (per unit cable length), L ≈ 100 m, d = 5 m d/L = 5/100 = 0.05 < 0.1 → parabolic approximation is valid For catenary with small sag: treat it as parabola with w in the formula: H ≈ wL²/(8d) = 0.5 × (100)² / (8 × 5) = 0.5 × 10000/40 = 125 kN Vertical reaction at support: V ≈ wL/2 = 0.5 × 100/2 = 25 kN (Note: For a true catenary, V = ws/2 where s is half the cable arc length. For small sag, s ≈ L/2, so V ≈ wL/2 — same result.) T_max = √(H² + V²) = √(125² + 25²) = √(15625 + 625) = √16250 = 127.5 kN Answer: T_max ≈ 127.5 kN (Note: Minimum tension at crown = H = 125 kN)

The parabolic equation y = (w/2H)x² is the shape equation with origin at the crown. This form is directly useful when the board exam asks for 'the position where the cable reaches a given elevation' or 'the clearance at a given location.'

Scenario

A cable with H = 500 kN supports a UDL of w = 8 kN/m on a 60 m span. At what horizontal distance from the crown does the cable elevation equal the crown plus 3 m?

Solution

Given: H = 500 kN, w = 8 kN/m, L = 60 m, y = 3 m Verify sag: d = wL²/(8H) = 8×3600/(8×500) = 28800/4000 = 7.2 m Parabolic equation (origin at crown, lowest point): y = (w/(2H))·x² = (8/(2×500))·x² = (8/1000)·x² = 0.008x² Solving for x when y = 3 m: 3 = 0.008x² x² = 3/0.008 = 375 x = √375 = 19.36 m from the crown Answer: x = 19.4 m from the midspan crown

Applications

  • Suspension bridge cable design — DPWH bridge design guidelines require computation of cable tension under dead load + live load.
  • Electrical transmission lines — PEC (Philippine Electrical Code) requires minimum ground clearance; sag calculation uses catenary formulas.
  • Cable-stayed roof structures — parabolic cable shape under ponding load.
  • Ropeway and aerial tramway cables — Tmax must be checked against cable rated breaking strength.
  • Pipeline river crossings — the pipeline acts as a catenary/parabolic cable under its own weight in water.

Misconceptions

  • WRONG: 'A cable loaded by its own weight forms a parabola.' — CORRECT: Self-weight (per unit cable length) → catenary. Deck load (per unit horizontal distance) → parabola. For small sag, they are nearly equal.
  • WRONG: 'H increases with sag for fixed span and load.' — CORRECT: H = wL²/(8d). LARGER sag d → SMALLER H. The cable is 'less stressed' horizontally when it hangs lower.
  • WRONG: 'T_max is at midspan.' — CORRECT: T_max is at the supports (steepest point). T_min = H at the crown.
  • WRONG: 'For a level cable (d → 0), tension approaches zero.' — CORRECT: For d → 0, H → ∞. A perfectly horizontal loaded cable would require infinite tension — physically impossible.
  • WRONG: 'The parabolic cable formula applies only to suspension bridges.' — CORRECT: It applies to any cable with load uniform per horizontal distance — e.g., horizontal conveyor cables, horizontal loading.

Related Concepts

  • Catenary curve — mathematical definition using hyperbolic cosine
  • Parabola — conic section, shape of uniformly horizontally loaded cable
  • Virtual work for cables — alternative derivation of cable equations
  • Suspension bridge design — main cable, hangers, stiffening truss/girder
  • Cable sag and clearance requirements — PEC, DPWH bridge standards

Common Exam Questions

Example

Span = 100 m, sag = 10 m, w = 5 kN/m. H = 5×10000/80 = 625 kN; V = 250 kN; T_max = √(625²+250²) = 672 kN.

Approach

Directly apply H = wL²/(8d) and T_max = √[H² + (wL/2)²].

Question Type

Find H and T_max for a parabolic cable

Example

w = 3 kN/m, L = 50 m, H = 400 kN. d = 3×2500/(8×400) = 7500/3200 = 2.34 m.

Approach

Rearrange parabolic formula: d = wL²/(8H).

Question Type

Find the sag given H and loading

Example

At x = L/4 from crown: y = (4d/L²)(L/4)² = (4d/L²)(L²/16) = d/4. Elevation at quarter-span = crown elevation + d/4.

Approach

Use y = (4d/L²)x² with origin at midspan crown, or y = (w/2H)x².

Question Type

Find the cable elevation at a specific point

Key Points To Remember

  • Uniform load per horizontal distance → Parabolic cable. H = wL²/(8d).
  • Uniform load per cable length → Catenary. For shallow cables (d/L < 0.1), use parabolic formula as approximation.
  • H = wL²/(8d): memorize this. It appears directly in CE Board problems.
  • T_max at supports = √[H² + (wL/2)²] — the Pythagorean combination of H and V.
  • Minimum tension is at the crown (lowest point) = H (horizontal component only).
  • Cable length: S ≈ L[1 + (8/3)(d/L)²] for approximate calculation.
  • For the CE Board: READ the problem carefully — 'per meter of span' (parabola) vs 'per meter of cable' (catenary).
  • Sag-to-span ratio d/L = wL²/(8H·L) = wL/(8H): larger load or longer span → more sag for given H.

Practice Problems

This problem reinforces the distinction between a frame (multi-force members) and a truss (all two-force members). When all members have loads only at their end joints, use truss analysis. The load is directly over A, so diagonal BC carries zero force — a classic 'zero-force member' scenario. Always check: if a joint has only two members and no external load (except at B here where By = 0), one or both may be zero-force members.

Problem

FRAME PROBLEM: A triangular frame consists of members AB (horizontal, 4 m long), BC (vertical, 3 m tall), and AC (diagonal). The frame is pinned at A (bottom left) and B (bottom right). A vertical load of 20 kN is applied at joint C (top left). Members AB is the base, BC is the left vertical, AC is the diagonal from top-left to bottom-right. Identify which members are two-force members and find the force in each member.

Solution

Step 1 — Identify two-force members: • Member AB: Connected at A and B. The pin at A is also a support — two reaction components. The load at C is NOT on AB. However, A is a support with two unknown reaction components, so AB has forces at A, B, and potentially a reaction at A — this needs more careful inspection. • Actually, redraw: A(0,0) is pin support. B(4,0) is pin support. C(0,3) has 20 kN downward load. Members: AB (A to B, horizontal), BC (B to C, diagonal from (4,0) to (0,3)), AC (A to C, vertical from (0,0) to (0,3)). Step 2 — Whole-body equilibrium: ΣMA = 0: By(4) − 20(0) = 0 → By = 0 (The 20 kN load is directly above A, so no moment about A from it.) ΣFy = 0: Ay + By − 20 = 0 → Ay = 20 kN ΣFx = 0: Ax + Bx = 0 Step 3 — Member AC (vertical, A(0,0) to C(0,3)): Loaded at C with 20 kN. Also connected at A. This is a TWO-force member? No — C has an external load, so AC is NOT a two-force member if we consider the 20 kN as applied at C. However, in the context of the frame, C is a JOINT. At joint C, the 20 kN is applied, and forces from members AC and BC meet. So AC and BC are two-force members (each connected at two joints with no intermediate loads); the 20 kN is at the JOINT, not ON a member. In this case, ALL three members are two-force members (this is actually a truss!): • AC: vertical, F_AC = internal axial force along AC direction (vertical) • BC: diagonal from B(4,0) to C(0,3), length = √(16+9) = 5 m, direction: (-4/5, +3/5) • AB: horizontal Joint C — ΣFy = 0: F_AC + F_BC·(3/5) − 20 = 0 Joint C — ΣFx = 0: F_BC·(-4/5) = 0 → F_BC = 0 From ΣFy: F_AC = 20 kN (compression, pushing C downward) Joint B — F_BC = 0, so: Bx = 0, By = 0 ✓ Joint A — F_AC = 20 kN (acts along AC): Ax = 0, Ay = 20 kN ✓ Answer: F_AC = 20 kN compression; F_BC = 0; F_AB = 0 Board-exam lesson: When the load is at a joint and all members are two-force, use method of joints from truss analysis.

This is the canonical frame problem for the CE Board Exam. The steps are: (1) recognize the two-force member (strut BC), determine its force direction, (2) draw the beam FBD with the strut force at C, (3) take moments about A to find F_BC directly, (4) use ΣF equations to find the pin reaction at A. The sign of Ay (downward) means the wall pin pulls the beam down — this is possible because it is a pin (can exert tension or compression).

Problem

FRAME PROBLEM (MULTI-FORCE): A horizontal beam AD (length 6 m) is pinned at wall at A(0,0). It carries a 15 kN load at D(6,0). A strut connects C(4,0) on the beam to B(0,−3) on the wall. Strut BC is a two-force member. Find: (a) force in strut BC, (b) pin reaction at A.

Solution

Step 1 — Geometry of strut BC: From B(0,−3) to C(4,0). Length = √(4²+3²) = 5 m. Direction cosines: l = 4/5 = 0.8 (x-direction), m = 3/5 = 0.6 (y-direction) Strut BC is in compression (pushes C toward beam at 45° from geometry). Step 2 — FBD of beam AD: At A: Ax (→) and Ay (↑) At C: strut force F_BC pushes beam at angle: horizontal component = F_BC×(4/5) pointing left (−x), vertical component = F_BC×(3/5) pointing upward (+y). [Strut pushes UP and to the LEFT on the beam.] At D: 15 kN downward (−y) Step 3 — ΣMA = 0 (eliminate Ax and Ay): (F_BC × 3/5)(4) − 15(6) = 0 F_BC × (12/5) = 90 F_BC = 90 × 5/12 = 37.5 kN Step 4 — ΣFy = 0: Ay + F_BC×(3/5) − 15 = 0 Ay = 15 − 37.5×0.6 = 15 − 22.5 = −7.5 kN → 7.5 kN downward Step 5 — ΣFx = 0: Ax − F_BC×(4/5) = 0 Ax = 37.5×0.8 = 30 kN (→, toward the beam, i.e., away from wall) Step 6 — Resultant at A: RA = √(30² + 7.5²) = √(900 + 56.25) = √956.25 = 30.9 kN Answer: F_BC = 37.5 kN (compression); RA = 30.9 kN at A (directed at arctan(7.5/30) = 14.04° below horizontal)

The key step is using the moment equation about the load point C for the left cable segment to find H. This eliminates the vertical force at C (the 25 kN load acts at C itself, but we take moments of the LEFT portion, so only VA and H appear). The left segment is steeper (shorter horizontal, same vertical drop), so it has the larger tension — consistent with 'max tension at steepest segment.'

Problem

CABLE PROBLEM: A cable spans 30 m between two supports at the same elevation. A single concentrated load of 25 kN hangs at a point 10 m from the left support. The sag at the load point is 3 m. Find: (a) H, (b) tension in the left segment, (c) tension in the right segment, (d) support reactions.

Solution

Step 1 — Geometry: Left support A(0,0), Load point C(10,−3), Right support B(30,0). Step 2 — FBD of entire cable: At A: H → (rightward) and VA ↑ At B: H → (leftward) and VB ↑ Load: 25 kN ↓ at x = 10 m Step 3 — ΣMB = 0: VA(30) − 25(30−10) = 0 VA(30) = 25(20) = 500 VA = 500/30 = 16.67 kN Step 4 — ΣFy = 0: VA + VB = 25 → VB = 25 − 16.67 = 8.33 kN Step 5 — Find H using geometry at load point C: Consider the left portion of cable (from A to C): ΣM at C = 0 for left portion: VA(10) − H(3) = 0 [H acts horizontally, moment arm = sag = 3 m] H = VA×10/3 = 16.67×10/3 = 55.57 kN Step 6 — Tension in left segment AC: Slope of AC: from A(0,0) to C(10,−3) tan θ_L = 3/10 = 0.3; θ_L = 16.70°; cos θ_L = 0.9578; sin θ_L = 0.2873 T_AC = H/cos θ_L = 55.57/0.9578 = 58.02 kN Check: T_AC × sin θ_L = 58.02 × 0.2873 = 16.67 kN = VA ✓ Step 7 — Tension in right segment CB: Slope of CB: from C(10,−3) to B(30,0) Horizontal: 20 m; Vertical: +3 m rise tan θ_R = 3/20 = 0.15; θ_R = 8.53°; cos θ_R = 0.9889; sin θ_R = 0.1490 T_CB = H/cos θ_R = 55.57/0.9889 = 56.19 kN Check: T_CB × sin θ_R = 56.19 × 0.1490 = 8.37 ≈ 8.33 kN = VB ✓ (rounding) Answer: H = 55.6 kN; T_AC = 58.0 kN (left, steeper); T_CB = 56.2 kN (right, shallower); VA = 16.67 kN; VB = 8.33 kN

This is a design-oriented problem typical in the higher-difficulty CE Board questions. The insight is that LARGER sag means LESS tension. The minimum sag corresponds to the maximum tension. Set T_max equal to the allowable value and solve for d. The vertical reaction V = wL/2 is fixed (independent of sag), so you only need to find H.

Problem

PARABOLIC CABLE: A suspension bridge cable spans 200 m between towers of equal height. The roadway load is 12 kN/m of horizontal span. The maximum allowable cable tension is 2000 kN. Determine the minimum sag required.

Solution

Given: L = 200 m, w = 12 kN/m, T_max ≤ 2000 kN Step 1 — Express T_max in terms of d: H = wL²/(8d) = 12(200²)/(8d) = 12×40000/(8d) = 480000/(8d) = 60000/d V = wL/2 = 12×200/2 = 1200 kN T_max = √(H² + V²) = √[(60000/d)² + 1200²] Step 2 — Set T_max = 2000 kN (limiting condition): √[(60000/d)² + 1200²] = 2000 (60000/d)² + 1440000 = 4000000 (60000/d)² = 2560000 60000/d = √2560000 = 1600 d = 60000/1600 = 37.5 m Step 3 — Verify: H = 60000/37.5 = 1600 kN T_max = √(1600² + 1200²) = √(2560000 + 1440000) = √4000000 = 2000 kN ✓ Answer: Minimum sag d = 37.5 m Note: Larger sag → smaller H and smaller T_max. The 37.5 m sag is the MINIMUM sag (corresponding to maximum allowable tension). Any sag less than 37.5 m would result in T_max exceeding 2000 kN.

The toggle press amplifies force as the links approach horizontal (θ → 0°). This is a machine problem where the M.A. = 1/(2 tan θ) varies dramatically with angle. The board exam may ask for the force at a specific angle or the angle that gives a required M.A. The key is the FBD at the central pin with the two link forces and the applied/output forces.

Problem

MACHINE PROBLEM: A toggle press mechanism has two equal links, each 200 mm long. The links are connected to a central pin that slides vertically, and their outer ends are pinned horizontally 300 mm apart (so each link makes an angle θ with the horizontal). A horizontal effort F = 500 N is applied at the central pin pushing it downward. When the links make θ = 20° with the horizontal, find the compressive force P on the workpiece below the central pin.

Solution

Step 1 — Geometry: Each link has length 200 mm. Horizontal spread = 300 mm total (150 mm each side from center). cos θ = 150/200 = 0.75, so θ = 41.41° Wait — re-read: links make θ = 20° with horizontal (given directly). So: θ = 20° sin 20° = 0.342, cos 20° = 0.940 Step 2 — FBD of the central pin (joint): The 500 N force pushes DOWN (this is the effort). Two link forces (compression) act along each link — each at 20° above horizontal (pushing outward and upward on the central pin from the fixed outer pins). Wait — if the outer pins are fixed and the effort pushes the central pin downward, the links push UPWARD on the fixed pins and the reaction on the central pin from each link acts at 20° UPWARD from horizontal. Actually, for a toggle press: effort is typically HORIZONTAL to push links toward horizontal. Let me use the standard toggle: For a TOGGLE CLAMP with two links at angle θ to horizontal: Relating vertical output force P to horizontal input force F: FBD of central joint: Two link forces T at angle θ from horizontal. Vertical: 2T sin θ = P Horizontal: The input is applied as the links are pushed toward flat (but for this problem, let F = 500 N be the downward force). For downward input F pushing central pin down, equilibrium of central pin: 2T sin θ = F (vertical equilibrium, links slope upward from center to outer pins) T = F/(2 sin θ) = 500/(2×0.342) = 500/0.684 = 730.9 N The output compressive force on the workpiece = P = 2T cos θ × tan(90°−θ)... let me redo with correct model. Standard toggle press: Input = horizontal force H_in at the elbow. Output = vertical force P at central pin (downward). This gives P = H_in/(2 tan θ). But if F is already defined as the downward force: Actually simplest approach — for a symmetric toggle with 2 links of equal length, each at angle θ to horizontal, with outer pins fixed horizontally: If effort P (downward) at elbow, it drives vertical displacement. At elbow joint: 2T sin θ = P (vertical), so T = P/(2 sin θ) Horizontal spread reaction at outer pins = 2T cos θ = P cos θ/sin θ = P/tan θ If instead F = 500 N is a DOWNWARD applied force at the central pin and we want the HORIZONTAL REACTION at the outer pins: Horizontal force per outer pin = T cos θ = 500cos20°/(2sin20°) = 500(0.940)/(2×0.342) = 470/0.684 = 687 N For a toggle clamp where the OUTPUT is horizontal clamping force: P_clamp = F/(2 tan θ) = 500/(2×tan20°) = 500/(2×0.364) = 500/0.728 = 686.8 N ≈ 687 N Answer: Clamping/reaction force = 687 N. M.A. = P/F = 687/500 = 1.37 at θ = 20° Note: As θ → 0° (links become horizontal), P → ∞ — this is the toggle action principle. At θ = 5°: M.A. = 1/(2tan5°) = 1/(2×0.0875) = 5.7; at θ = 1°: M.A. = 28.6.

Exam Preparation Tips

  • MASTER THE THREE-PHASE FRAME SOLUTION: (1) Identify two-force members, (2) Find external reactions from whole-body FBD, (3) Dismember and apply ΣFx=0, ΣFy=0, ΣM=0 to each member. Practice this sequence until it is automatic.
  • MEMORIZE THE CABLE FORMULAS: H = wL²/(8d) for parabolic cable; T_max = √[H² + (wL/2)²]; T = H/cos θ at any point. These three formulas cover ~80% of CE Board cable questions.
  • KNOW THE DIFFERENCE — PARABOLA vs CATENARY: Read the problem statement. 'Uniform load per meter of span' or 'deck load' → parabola. 'Cable weight per meter of cable' or 'self-weight' → catenary (use parabola approximation if d/L < 0.10).
  • TWO-FORCE MEMBER RECOGNITION: In every frame problem, scan all members before writing any equation. A two-force member reduces your unknowns by one (direction is known). Missing a two-force member is the most common student error.
  • NEWTON'S THIRD LAW AT PINS: At every shared pin, the force on member A equals the force on member B in magnitude but opposite in direction. Draw both FBDs and check that your pin force arrows are consistent.
  • MOMENT CENTER SELECTION: Always take ΣM about the point where the most unknowns have zero moment arm (usually where two unknowns intersect). This gives you one equation with one unknown.
  • CABLE MAXIMUM TENSION LOCATION: T_max is at the steepest cable segment — at the supports for level cables. T_min is at the crown (horizontal) = H. A common wrong answer on the board exam is placing T_max at midspan.
  • PARABOLIC CABLE SHAPE EQUATION: y = (4d/L²)x² with origin at midspan crown. Use this when the exam asks for cable elevation or clearance at a specific horizontal location.
  • CHECK UNITS CONSISTENTLY: Use kN for forces and meters for distances throughout. Mixing N and kN in H = wL²/(8d) is a common source of errors.
  • MECHANICAL ADVANTAGE USING MOMENTS: For any machine (lever, pliers, scissors), take ΣM = 0 about the pivot. The M.A. formula M.A. = effort arm / load arm is a direct consequence — derive it rather than memorize it blindly, to handle non-standard geometries.
  • CABLE WITH UNEQUAL SUPPORTS: If the two cable supports are at different elevations, use the general approach — assign coordinates to all key points, find vertical reactions from whole-body ΣM = 0 and ΣFy = 0, then use the sag geometry at any load point to find H.
  • PRACTICE THE 'H IS CONSTANT' CONCEPT: This is the single most important cable principle. In every cable problem, identify H first — it connects all segment tensions and is constant throughout. Use the moment equation about a load point: ΣM = 0 for the left or right cable portion to extract H elegantly.
  • REVIEW RELATED PAST BOARD EXAM PROBLEMS: CE Board cable problems typically involve spans of 20–100 m with sags of 2–10 m and UDLs of 5–20 kN/m. Frame problems commonly involve 3–6 m spans with loads of 10–50 kN. Calibrate your calculations to these typical magnitudes.
  • DURING THE EXAM — DRAW FIRST, CALCULATE SECOND: Spend the first 1–2 minutes sketching the free body diagram with all forces labeled before writing any equation. This prevents sign errors and missing forces.
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In summary

Frames, machines, and cables are three structurally distinct systems that every civil engineer must analyze fluently for the PRC CE Licensure Examination. The common thread across all three is the disciplined application of static equilibrium — but the context, key principles, and formulas differ importantly. For FRAMES: The three-phase approach (identify two-force members → whole-body reactions → dismember with Newton's Third Law) is non-negotiable. Rushing to dismember without first finding reactions, or treating a multi-force member as a two-force member, are the two errors that most frequently cost points on the board exam. For MACHINES: The mechanical advantage relationship (M.A. = effort arm / load arm) comes directly from ΣM = 0 about the pivot. Understand it as an equilibrium result, not just a formula to memorize. Remember that the toggle mechanism's M.A. = 1/(2 tan θ) becomes very large as θ → 0°. For CABLES: Two principles govern all cable problems regardless of loading type: (1) H is constant throughout the cable, and (2) maximum tension is at the steepest point (supports for level cables). The parabolic formula H = wL²/(8d) is one of the most exam-frequently-tested formulas in Engineering Mechanics — know it precisely, and know when it applies (uniform load per horizontal distance). For self-weight (load per cable length), use the catenary formulas or the parabolic approximation when d/L < 0.10. Mastery of these three topics requires both conceptual clarity and computational skill. Draw every free body diagram before writing any equation. Use moment equations strategically to decouple unknowns. And always verify your answers using an unused equilibrium equation — a simple but powerful habit that catches arithmetic errors before they become wrong answers. With systematic practice of the worked examples and practice problems in this chapter, you will be well-prepared to answer frames, machines, and cables problems confidently on examination day.

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