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CELE Engineering MechanicsFrames, Machines and CablesRevision Notes

Revision notes for CELE Engineering Mechanics — Frames, Machines and Cables. Short, focused, and designed for the week before exam day. Use these when you are already familiar with the chapter and need a quick refresh on the high-yield items Professional Regulation Commission (PRC) — Board of Civil Engineering tests.

Exam context

The Civil Engineer Licensure Examination is conducted by Professional Regulation Commission (PRC) — Board of Civil Engineering and is scheduled for May and November 2026. The Engineering Mechanics subtest is marked as "Core" in the official pattern, and Frames, Machines and Cables appears in position 4th of 8 in the CELE Engineering Mechanics review rotation. Passing mark: 70% weighted average, no sub-test below 50%. Recent CELE 2026 papers have drawn roughly a meaningful share of questions from this subject.

Frames, Machines and Cables - Revision Notes

Frames, machines, and cables are three fundamental structural systems that appear regularly in the PRC Civil Engineer Licensure Examination under Engineering Mechanics. Unlike trusses — which consist entirely of two-force members carrying only axial loads — frames and machines contain at least one multi-force member that develops shear, bending, and axial effects simultaneously. Cables represent the other extreme: perfectly flexible tension-only members that adopt a geometry governed entirely by the applied loading. Mastery of these three systems requires confident application of free-body diagrams (FBDs), Newton's third law at shared pins, identification of two-force members, and the parabolic cable equations. This chapter consolidates every concept, formula, and pitfall examiners test in board-style problems.

Sections

Formulas

Example

Beam AB (6 m, pinned at A, load 12 kN at B, strut CD at midpoint C at 45°): ΣM_A = 0 → (F_CD sin45°)(3) = 12(6) → F_CD = 33.9 kN compression.

Formula

ΣFx = 0, ΣFy = 0, ΣM_O = 0

Variables

ΣFx = sum of horizontal forces; ΣFy = sum of vertical forces; ΣM_O = sum of moments about any convenient point O

Application

Applied to the FBD of the whole frame to find external reactions, and again to each dismembered member to find internal pin forces.

Example

From the solved beam example: A_x = –24 kN, A_y = –12 kN → R_A = √(24² + 12²) = 26.8 kN.

Formula

R_A = √(A_x² + A_y²)

Variables

R_A = resultant pin reaction at A; A_x, A_y = horizontal and vertical components of the pin reaction

Application

Used after solving component equations to find the magnitude of a pin reaction.

Exam Tips

  • Start every frame problem by scanning for two-force members — they are usually straight members with pins only at both ends and no loads in between. Label them immediately.
  • Choose your moment equation point wisely: a pin shared by two unknown force components eliminates both with one equation.
  • Check your answer: the pin forces on a dismembered member must satisfy all three equilibrium equations independently.
  • In multiple-choice items, if four unknowns appear at a single pin but only three equations are available per member, look for additional two-force members or use the whole-frame FBD first.
  • Boards often ask for the 'force in strut CD' — this is the magnitude of the two-force member reaction, so remember to divide by the appropriate trig function.

Key Points

  • A frame is a stationary structure designed to support loads; it contains at least one multi-force member (a member loaded at more than two points, or carrying an applied moment).
  • Multi-force members carry shear, bending moment, and axial force — NOT axial force alone.
  • A two-force member is loaded ONLY at two points with no transverse loads between them; its resultant force must act along the line joining the two points.
  • Identify two-force members first — they reduce unknowns immediately by fixing the direction of the pin force.
  • Step 1: Draw the FBD of the entire frame and find external reactions using ΣFx = 0, ΣFy = 0, ΣM = 0.
  • Step 2: Dismember the frame — draw a separate FBD for each individual member.
  • Step 3: At every shared pin, apply Newton's third law — the force on member A from member B is equal in magnitude and opposite in direction to the force on member B from member A.
  • Step 4: Apply three equilibrium equations to each member and solve for pin forces.
  • The total number of unknowns must equal the total number of equilibrium equations available.

Definitions

Term

Multi-force member

Definition

A structural member that is subjected to three or more forces, or to two forces and at least one couple/moment. It cannot be treated as a simple two-force member.

Importance

Critical — if you incorrectly treat a multi-force member as a two-force member, every subsequent calculation will be wrong. Board exams frequently test this distinction.

Term

Two-force member

Definition

A member in equilibrium under exactly two forces applied at two separate points, with no other loads between them. The two forces must be equal, opposite, and collinear (directed along the member axis).

Importance

Identifying two-force members instantly gives you the direction of the pin force, cutting unknowns from 2 (Cx, Cy) to 1 (F along the member). Essential for efficiency in board exams.

Term

Dismembering (method of members)

Definition

The process of separating a frame or machine into its individual members, drawing a complete FBD for each, and applying equilibrium equations to find internal pin forces.

Importance

This is the standard analysis method for all frames and machines in the licensure exam.

Term

Newton's Third Law at pins

Definition

If member A exerts a force F on member B at their shared pin, then member B exerts an equal, opposite force –F on member A. Both forces must appear when you dismember.

Importance

Forgetting to reverse the direction of pin forces on the paired member is the single most common error in frame problems on board exams.

Section Title

Frames — Stationary Multi-Force Structures

Common Mistakes

  • Labeling a member as two-force when it carries a transverse load or has three pin connections — always count the number of force application points first.
  • After dismembering, drawing pin forces in the same direction on both members instead of reversing (violating Newton's third law).
  • Taking moments about a point that introduces two unknowns — always select a point that eliminates as many unknowns as possible (e.g., a pin location).
  • Forgetting to include the weight of members if specified — self-weight acts at the centroid and makes a member multi-force.
  • Treating the entire frame as a single rigid body when computing internal pin forces — you must dismember it.

Formulas

Example

Effort arm = 0.4 m, load arm = 0.05 m, effort = 50 N → Load = 50 × (0.4/0.05) = 400 N. M.A. = 8.

Formula

M.A. = Load / Effort = Effort Arm / Load Arm (lever)

Variables

M.A. = mechanical advantage (dimensionless); Load = output force (N or kN); Effort = input force (N or kN); Effort arm = perpendicular distance from pivot to effort line of action (m); Load arm = perpendicular distance from pivot to load line of action (m)

Application

First-class levers (fulcrum between effort and load), second-class levers (load between effort and fulcrum), and third-class levers (effort between load and fulcrum). Board exams use all three.

Example

Pliers: pivot at C. Jaw force Q at distance a, hand force P at distance b. ΣM_C = 0 → Q(a) = P(b) → Q = P(b/a).

Formula

ΣM_pivot = 0 → F_load × d_load = F_effort × d_effort

Variables

F_load = load force; d_load = moment arm of load about pivot; F_effort = applied effort; d_effort = moment arm of effort about pivot

Application

Used for any machine linkage or lever to find either the load or the effort by taking moments about the pivot/pin.

Example

An ideal pulley system with M.A. = 4 and η = 80%: actual load lifted = 0.80 × (4 × Effort).

Formula

η = (Load × load displacement) / (Effort × effort displacement) × 100%

Variables

η = efficiency (%); Load displacement = how far the load moves; Effort displacement = how far the effort moves

Application

Applied when friction or energy losses are considered. For an ideal (frictionless) machine, η = 100%.

Exam Tips

  • For a machine problem, first write ΣM about the pivot/pin to get the load-effort relationship directly — this is usually the fastest path to the answer.
  • Identify whether the pivot is a fixed pin or a moving pin, as this affects the FBD.
  • If the problem gives geometry (lengths and angles), resolve forces into components before taking moments.
  • Board examiners frequently test pliers and toggle clamps — practice both by dismembering at the pivot and applying ΣM = 0 to one jaw.

Key Points

  • A machine is a structure with moving parts designed to transmit or modify forces (e.g., pliers, toggle clamp, hydraulic press, crane hook, scissors, wheel-and-axle).
  • Analysis method is identical to frames: dismember → FBD of each part → apply equilibrium.
  • The key output of a machine analysis is the relationship between the effort (input force) and the load (output force), called the mechanical advantage (M.A.).
  • Mechanical advantage > 1 means the machine amplifies force (effort arm > load arm for a lever).
  • For a simple lever: M.A. = effort arm / load arm. If M.A. = 8, a 50 N effort lifts 400 N.
  • For a pulley system: M.A. equals the number of rope segments supporting the load.
  • In compound machines, multiply the M.A. of each stage.
  • Efficiency η = (actual load) / (ideal load) — real machines have friction losses so η < 1.
  • Board problems on machines most commonly involve levers, pliers, toggle clamps, and cranes.

Definitions

Term

Mechanical advantage (M.A.)

Definition

The ratio of the output force (load) to the input force (effort). For an ideal machine it equals the ratio of the effort moment arm to the load moment arm.

Importance

Directly tested in board exam problems involving levers, pliers, and pulley systems. Always verify units cancel — M.A. is dimensionless.

Term

Effort arm

Definition

The perpendicular distance from the fulcrum (pivot) to the line of action of the applied effort force.

Importance

Confusion between effort arm and effort distance along the lever is a common source of error.

Term

Mechanical efficiency

Definition

The ratio of useful work output to work input, expressed as a percentage. Real machines have efficiency less than 100% due to friction.

Importance

Occasionally tested in problems involving real machines where friction is specified.

Section Title

Machines — Force Transmission and Mechanical Advantage

Common Mistakes

  • Using the total length of the lever instead of the perpendicular moment arm — always use the perpendicular distance to the line of action of the force.
  • Confusing the class of lever, which changes where the fulcrum, effort, and load are located.
  • Forgetting that a machine must also be dismembered at its pins for complete internal force analysis — the overall moment equation gives the load-effort relationship, but pin forces require the full FBD of each part.
  • Not accounting for efficiency when the problem states a friction coefficient or percent efficiency.
  • For pliers/scissors: treating the joint as a single body instead of two separate members connected at a pivot.

Formulas

Example

w = 6 kN/m, L = 40 m, d = 4 m → H = 6(40²)/(8×4) = 6(1600)/32 = 300 kN.

Formula

H = wL² / (8d)

Variables

H = horizontal tension component (kN, constant throughout the cable); w = uniformly distributed load per unit horizontal length (kN/m); L = horizontal span (m); d = sag at midspan (m)

Application

Used for suspension bridge cables or any cable under uniform horizontal load — the parabolic cable formula. This is the most frequently tested cable formula in the CE board exam.

Example

H = 300 kN, wL/2 = 6(40)/2 = 120 kN → T_max = √(300² + 120²) = √(90000 + 14400) = √104400 = 323.1 kN.

Formula

T_max = √(H² + (wL/2)²)

Variables

T_max = maximum cable tension (kN), occurring at the supports for a symmetric cable; H = horizontal tension component (kN); wL/2 = vertical reaction at each support (kN) for a symmetric loading

Application

Finds the maximum tension (at the cable supports) once H is known. The vertical component at the support equals wL/2 for a symmetric, uniform horizontal load.

Example

Cable at midspan carrying a single central load, sag = 1.5 m, half-span = 6 m → tan θ = 1.5/6 = 0.25 → θ = 14.04° → T = H/cos14.04°.

Formula

T = H / cos θ

Variables

T = tension at any point along the cable (kN); H = horizontal component (kN, constant); θ = angle of the cable tangent with the horizontal at that point (degrees)

Application

Finds tension at any specified location once the cable angle θ is known. Used for both concentrated-load cables and parabolic cables.

Example

At support (x = L/2 = 20 m from midspan): tan θ = (6×40/2)/300 = 120/300 = 0.4 → θ = 21.8° (angle of cable at support).

Formula

tan θ = (wL/2 ± wx) / H (parabolic cable, origin at midspan)

Variables

θ = cable angle at horizontal distance x from midspan; w = uniform horizontal load; L = span; H = horizontal tension component; + for right side, – for left

Application

Gives the cable slope at any point for a parabolic cable. Used to find the angle at the supports or at any specified section.

Example

Single load P = 10 kN at midspan, span L = 12 m, sag d = 1.5 m. Half-span = 6 m. ΣM at load point → 2T sin θ = 10 kN → T = 10/(2 × 0.2425) = 20.6 kN.

Formula

For concentrated loads: ΣM = 0 at each load point to find sag; H is constant

Variables

H = horizontal component (constant); sag y_i at load point i found from moment equation of the cable segment to the left or right of the load.

Application

Applied to cables with one or more concentrated loads. Cut the cable at the load point, draw FBD of the segment, and write ΣM = 0 at the load point.

Exam Tips

  • Always identify the loading type first: horizontal UDL → parabola (H = wL²/8d); self-weight → catenary (parabola approximation OK for shallow sag); point loads → funicular polygon.
  • Find H first using ΣM about a support — H is the same everywhere and simplifies all subsequent calculations.
  • For a parabolic cable, the vertical reaction at each support for a symmetric loading equals wL/2, making T_max computation straightforward.
  • In board exam problems, the answer choices for T_max are often close — carry at least four significant figures through your calculation before rounding.
  • For a cable with unequal support elevations, use a Cartesian coordinate system with the origin at one support, and write the moment equation at a point to find H — the procedure is the same but the geometry is asymmetric.

Key Points

  • A cable is perfectly flexible — it has no bending stiffness. It carries ONLY tension (no compression, no shear, no bending moment).
  • The tension in a cable is always directed tangentially along the cable at any point.
  • The HORIZONTAL COMPONENT of cable tension H is CONSTANT throughout the cable's length (for any loading — this follows from ΣFx = 0 applied to any free-body cut of the cable).
  • The maximum tension occurs at the steepest point — for symmetric loading this is at the supports, NOT at midspan.
  • THREE LOADING CASES: (1) Concentrated loads → funicular polygon (straight segments between loads); (2) Uniform load per horizontal distance → parabola; (3) Uniform load along cable length (self-weight) → catenary.
  • For shallow sag (sag/span < 0.1), the catenary is well approximated by the parabola.
  • For a cable with concentrated loads: the sag at each load point is found by solving moment equations at the load points.
  • At any load point: the change in cable slope equals the applied load divided by H.

Definitions

Term

Sag (d)

Definition

The vertical distance from the chord connecting the two supports down to the lowest point of the cable. For a symmetric cable with both supports at the same elevation, the sag occurs at midspan.

Importance

Sag is the primary geometric parameter in cable problems. It appears in both H = wL²/8d and in trigonometric computations for concentrated-load cables.

Term

Horizontal tension component (H)

Definition

The horizontal projection of the cable tension at any cross-section. It is constant throughout the entire cable length regardless of loading pattern, as long as no horizontal external forces are applied along the cable.

Importance

The constancy of H is the most powerful tool in cable analysis — board problems are almost always solved by finding H first, then using T = H/cos θ.

Term

Parabolic cable

Definition

The shape taken by a cable under a load that is uniformly distributed per unit horizontal distance (e.g., the deck weight of a suspension bridge). Described by y = wx²/(2H) with origin at midspan.

Importance

The parabola is the dominant cable shape tested in board exams. The catenary (uniform load along cable length) is rarely tested quantitatively at this level.

Term

Catenary

Definition

The shape taken by a cable under its own self-weight (load uniform along the arc length). Described by the hyperbolic cosine y = a(cosh(x/a) – 1). For small sag-to-span ratios, it closely approximates a parabola.

Importance

Know the distinction conceptually — board exams test whether you know WHICH shape applies to which loading condition, even if the catenary formula itself is rarely computed.

Term

Funicular polygon

Definition

The shape of a cable loaded by a finite number of concentrated loads. The cable consists of straight segments between the load points, and the shape resembles a polygon.

Importance

Used when a cable carries discrete point loads (e.g., two loads at the third points). Each segment is straight; H is still constant.

Section Title

Cables — Concentrated Loads and Parabolic Cables

Common Mistakes

  • Assuming maximum tension occurs at midspan — it occurs at the SUPPORT (steepest point) for a symmetric parabolic or concentrated-load cable.
  • Using the arc length of the cable instead of the horizontal span L in the formula H = wL²/8d — L is always the HORIZONTAL span.
  • Assuming sag and H are independent — they are inversely related: deeper sag means lower H and lower tension.
  • Forgetting that H is constant — some students recompute H at every point when only T (the resultant) changes along the cable.
  • Using the catenary formula for a uniformly distributed deck load (which is parabolic) or vice versa.
  • For cables with two loads at different sag values, incorrectly assuming the sag is at midspan — the geometry must be solved from ΣM = 0.

Formulas

Example

If whole-frame ΣFy = applied load – Ay – By = 0 was used to find reactions, verify each member's ΣFy = 0 separately after dismembering.

Formula

Complete Frame Check: ΣF_x(all members) = 0, ΣF_y(all members) = 0

Variables

Sum all x-forces and all y-forces across all dismembered members. Internal pin forces cancel in pairs (Newton's third law), leaving only the external forces.

Application

Used as a global check after solving all member equations. If external forces and reactions satisfy equilibrium of the whole frame, the solution is consistent.

Exam Tips

  • Allocate 4–5 minutes per frame/cable problem in the licensure exam. If a problem takes longer, skip and return — these problems are systematic once the FBD is correct.
  • In four-choice items, eliminate obviously wrong orders of magnitude first (e.g., a cable tension that is less than the applied load is physically impossible).
  • Memorize H = wL²/8d and T_max = √(H² + (wL/2)²) — these two equations solve 80% of parabolic cable board problems.
  • For frames, memorize the procedure: whole → dismember → Newton's third law at pins. Practice this sequence until it is automatic.

Key Points

  • A typical board problem involves 4–5 steps; the most common errors occur in setting up the FBD, not in the algebra.
  • Always state your sign convention clearly (positive x to the right, positive y upward, counterclockwise moments positive) and maintain it throughout.
  • For frame problems: whole-frame FBD → external reactions → dismember → member FBDs → pin forces.
  • For cable problems: identify cable type → find H → find T at required location using T = H/cos θ.
  • For machine problems: dismember at pivot → ΣM about pivot → load-effort relationship → M.A.
  • Verify: check that ΣFx = 0 and ΣFy = 0 on each FBD after solving — this is your built-in error check.
  • In the board exam, most cable and frame problems can be solved in under 5 minutes if the FBD is drawn correctly on the first attempt.

Definitions

Term

Free-body diagram (FBD)

Definition

A diagram of an isolated body (whole structure, individual member, or cable segment) showing all external forces and moments acting on it. The body is shown 'free' — cut away from all connections — and all forces at cut sections are shown explicitly.

Importance

The FBD is the foundation of every statics problem. An incorrect FBD guarantees an incorrect answer, regardless of how well the algebra is executed.

Section Title

Integrated Approach — Solving Board-Style Problems

Common Mistakes

  • Rushing to write equations without first drawing a complete, correct FBD — always draw first, compute second.
  • Mixing up the directions of force components when resolving at an angle — use a right-triangle diagram for each inclined force.
  • Rounding intermediate values too aggressively — carry at least four significant figures until the final answer.
  • Not verifying the solution against a remaining unused equilibrium equation — always use your third equation as a check.

Connections

  • Truss analysis (method of joints, method of sections) is a prerequisite — frames differ from trusses by having multi-force members, but the FBD and equilibrium principles are identical.
  • Shear and moment diagrams in Strength of Materials apply to multi-force beam members in frames — the internal forces at any section of a frame member are found by cutting the member and applying equilibrium.
  • Cable sag-tension relationships appear in structural analysis of suspension bridges, overhead transmission lines, and catenary overhead contact systems — directly relevant to Philippine infrastructure projects.
  • Mechanical advantage from machine analysis connects to the design of lifting equipment and rigging calculations governed by DOLE safety standards and AISC Design Guide references for crane runway design.
  • Newton's third law at pins is the same principle used in the stiffness method (matrix structural analysis) when assembling the global stiffness matrix from individual element stiffness matrices.
  • The funicular polygon for concentrated cable loads is geometrically equivalent to the load-path concept in arch analysis — the 'thrust line' of an arch is the inverted funicular polygon.
  • Hydrostatic forces on curved surfaces (fluid mechanics) use the same decomposition into horizontal and vertical components as cable tension analysis — connecting different topics in CE board review.
  • RA 544 (Civil Engineering Law) mandates that licensed civil engineers must competently apply structural analysis principles such as those in this chapter in the design and inspection of structures in the Philippines.

Exam Strategy

In the PRC Civil Engineer Licensure Examination, Frames, Machines and Cables problems appear in the Engineering Mechanics section and typically account for 3–6 items per exam. Prioritize the following: (1) CABLE PROBLEMS — memorize H = wL²/8d and T_max = √(H² + (wL/2)²) without hesitation; parabolic cable problems are the most consistent cable items. (2) FRAME DISMEMBERING — practice identifying two-force members rapidly, then draw clean FBDs. The moment equation about a pin eliminates two unknowns at once. (3) MACHINE M.A. — always take moments about the pivot to get the load-effort relationship in one equation. In multiple-choice format, work backward from the answer choices if the setup is complex — substitute each choice into the equilibrium equation and verify. Allocate 4 minutes per problem; if a frame problem requires more than 6 minutes, mark it and return after completing the rest. In the last 10 minutes of the exam, verify that your cable tension answers are always greater than the applied load (T > P for any loaded cable) as a sanity check.

Quick Review Questions

A horizontal beam is pinned at A and supported by a strut CD (a two-force member at 45°) at its midpoint C. A 12 kN downward load acts at the free end B, 6 m from A. The midpoint C is at 3 m from A. What is the compressive force in strut CD?

Taking moments about pin A on the beam FBD: ΣM_A = 0 → (F_CD × sin 45°)(3 m) = 12 kN × 6 m → F_CD × 0.7071 = 24 kN → F_CD = 24/0.7071 = 33.94 kN. The strut is a two-force member so its force acts at 45° along the strut. Because the strut pushes the beam upward (reaction), the strut itself is in compression.

A suspension cable spans 40 m horizontally with a midspan sag of 4 m. The cable supports a uniform horizontal load of 6 kN/m (parabolic cable). Calculate: (a) the horizontal tension H, and (b) the maximum cable tension T_max.

(a) H = wL²/(8d) = 6(40²)/(8×4) = 6(1600)/32 = 9600/32 = 300 kN. (b) Vertical reaction at each support V = wL/2 = 6(40)/2 = 120 kN. T_max = √(H² + V²) = √(300² + 120²) = √(90000 + 14400) = √104400 = 323.1 kN. Maximum tension occurs at the supports where the cable angle is steepest.

A lever has an effort arm of 0.4 m and a load arm of 0.05 m. What is the mechanical advantage, and what load does a 50 N effort balance?

M.A. = effort arm / load arm = 0.4 m / 0.05 m = 8. Load = Effort × M.A. = 50 N × 8 = 400 N. Alternatively from ΣM_pivot = 0: F_load(0.05) = 50(0.4) → F_load = 20/0.05 = 400 N.

A cable carries a single concentrated load of 10 kN at midspan. The horizontal span is 12 m and the cable sags 1.5 m at the load point. Find the cable tension.

Half-span = 6 m, sag = 1.5 m. Cable angle: tan θ = 1.5/6 = 0.25 → θ = 14.04°, sin θ = 0.2425, cos θ = 0.9701. By symmetry: ΣF_y = 0 at load point → 2T sin θ = 10 kN → T = 10/(2 × 0.2425) = 10/0.4851 = 20.6 kN. Also: H = T cos θ = 20.6 × 0.9701 = 20.0 kN (horizontal component, constant).

Why is the horizontal component of tension H constant throughout a cable, regardless of load position?

Consider any free-body segment of the cable cut at two sections. The only external forces are vertical (loads and reactions). For horizontal equilibrium: H_left = H_right. This must hold for every possible cut, so H is the same throughout the cable. This is a fundamental cable property — it is NOT true for the total tension T, which varies with the angle θ.

A cable is loaded by self-weight only (no deck load). What shape does it take, and when is it acceptable to approximate this shape as a parabola?

The catenary equation is y = a(cosh(x/a) – 1) where a = H/w (w = weight per unit arc length). For shallow sags (small d/L), the catenary and parabola are nearly identical numerically. For most civil engineering suspension structures under deck loads (uniform per horizontal meter), the true shape is parabolic — the catenary only applies when the cable carries its own weight primarily.

In the analysis of a frame, after dismembering, the pin force on member AB at pin C is found to act at 30° above the horizontal pointing to the right. What is the direction of the pin force at C acting on the other member BC?

Newton's third law: for every action, there is an equal and opposite reaction. The force that member BC exerts on AB is 30° above horizontal to the right. Therefore, the force that AB exerts on BC at the same pin must be 30° below horizontal to the left — same magnitude, reversed direction. This reversal must be applied every time you separate two members at a shared pin.

A parabolic cable with sag d is carrying uniform load w. If the sag is DOUBLED with the same span and load, what happens to H and T_max?

From H = wL²/(8d): if d doubles, H = wL²/(8 × 2d) = (1/2)(wL²/8d) → H is halved. The vertical component at each support V = wL/2 is unchanged (depends only on w and L, not sag). T_max = √(H² + V²) → with smaller H and same V, T_max decreases. This demonstrates that a deeper sag reduces cable tension — important for design optimization.

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