Frames, Machines and Cables - Study Notes
This chapter explores three fundamental structural systems in engineering mechanics: frames, machines, and cables. Unlike trusses (which consist solely of two-force members), frames and machines contain multi-force members that develop shear and bending in addition to axial force. Cables represent the opposite extreme—perfectly flexible structures carrying only tension and shape-shifting under load. Mastery of these topics is essential for the PRC Civil Engineer Licensure Examination, appearing regularly in structural analysis and mechanics problems. This chapter develops the analytical methods to solve these systems using equilibrium conditions and the free-body diagram (FBD) approach.
1. Frames: Concepts and Analysis
A frame is a stationary structure composed of members connected at pins or rigid joints, with at least one multi-force member (a member loaded at more than two points or carrying an applied moment). Unlike trusses, frames develop internal shear forces and bending moments in their members in addition to axial forces.
Key Distinction from Trusses:
Trusses are loaded only at joints and all members are two-force members; frames may have transverse loads on members themselves, creating internal moments and shears. This fundamental difference requires a different analysis approach.
Method of Analysis:
The standard approach involves two main steps:
- External Equilibrium: Apply equilibrium equations (ΣFx = 0, ΣFy = 0, ΣM = 0) to the entire frame as a free body to find the support reactions.
- Dismembering the Frame: Separate the frame into individual members, drawing a complete free-body diagram for each member. At each pin connection, apply Newton's third law—the force exerted by one member on an adjacent member is equal in magnitude but opposite in direction to the force exerted back.
Critical Identification: Always identify two-force members within the frame first. A two-force member (loaded only at its ends with no intermediate loads or moments) develops a force along its longitudinal axis. This immediately reduces unknowns. For example, if a frame contains a diagonal strut with pins only at its ends and no transverse loads, the force within it acts along the strut's axis.
Sign Convention and Direction: When dismembering, assume directions for pin forces (typically along positive x and y axes). Consistency is essential: if member AB exerts a rightward force on member BC at their shared pin, member BC exerts a leftward force on member AB at the same pin.
Examples
A horizontal beam AB is pinned to a wall at point A (0, 0) and extends to free end B (6, 0 m). A vertical load of 12 kN acts downward at the free end B. The beam is supported at its midpoint C (3, 0 m) by a strut CD running to the wall at D (0, −3 m). Determine: (a) the force in the strut CD, (b) the pin reaction at A, (c) verify that the strut is in compression or tension.
Answer
(a) Strut force Fs = 33.9 kN (compression). (b) Pin reaction at A: Ax = 24 kN (toward wall), Ay = 12 kN (downward), resultant RA = 26.8 kN. (c) The strut is in compression.
Solution
Step 1: Geometry of the strut.
The strut runs from C(3, 0) to D(0, −3), so its slope is −3/3 = −1, giving an angle of 45° below the horizontal (or 45° measured counterclockwise from the positive x-axis to the downslope direction).
Step 2: Dismember the frame.
The strut CD is a two-force member (loaded only at its ends C and D). The beam AB is a multi-force member (it carries the 12 kN load at B and receives support from the strut at C).
Step 3: Analyze the strut as a two-force member.
For a two-force member, the force must act along the member. At C, let the strut force be Fs directed from C toward D (compression assumption). This force has components:
- Horizontal: −Fs cos(45°) = −Fs(0.707) (leftward)
- Vertical: −Fs sin(45°) = −Fs(0.707) (downward)
By Newton's third law, the force exerted by the strut on the beam at C is equal and opposite:
- Horizontal: +Fs cos(45°) = +Fs(0.707) (rightward)
- Vertical: +Fs sin(45°) = +Fs(0.707) (upward)
Step 4: Apply equilibrium to the beam.
FBD of beam AB:
- Applied load: 12 kN downward at B
- Strut support: Fs cos(45°) rightward and Fs sin(45°) upward at C
- Pin reaction at A: Ax (horizontal) and Ay (vertical)
Moment equilibrium about A (taking counterclockwise as positive):
ΣMA = 0:
[Fs sin(45°)](3 m) − (12 kN)(6 m) = 0
Fs(0.707)(3) = 72
Fs(2.121) = 72
Fs = 33.9 kN
This is compression (the strut pushes at C, pushing the beam upward).
Vertical force equilibrium:
ΣFy = 0:
Ay + Fs sin(45°) − 12 = 0
Ay + 33.9(0.707) − 12 = 0
Ay + 24.0 − 12 = 0
Ay = −12 kN (i.e., 12 kN downward)
Horizontal force equilibrium:
ΣFx = 0:
Ax + Fs cos(45°) = 0
Ax + 33.9(0.707) = 0
Ax + 24.0 = 0
Ax = −24 kN (i.e., 24 kN toward the wall, or leftward)
Step 5: Magnitude of pin reaction at A.
RA = √(Ax² + Ay²) = √(24² + 12²) = √(576 + 144) = √720 = 26.8 kN
Verification: The strut is in compression at 33.9 kN. By Newton's third law, the strut exerts equal and opposite forces on the beam and wall, confirming consistency in the dismembered analysis.
A frame consists of three members: AB (horizontal), BC (vertical), and a diagonal member AC connecting them. Member AB is pinned to a wall at A and has a length of 4 m. Member BC is vertical, 3 m tall, and pinned to AB at B. Member AC connects A to C (a distance of 5 m). A horizontal load of 8 kN acts to the right at point C. Assume all joints are pinned and the frame is in equilibrium. Determine the forces in each member.
Solution
Step 1: Identify the geometry.
A is at the origin (0, 0). B is at (4, 0). C is at (4, 3). The distance AC is √[(4-0)² + (3-0)²] = 5 m (a 3-4-5 right triangle).
Step 2: External equilibrium.
Apply equilibrium to the entire frame:
ΣFx = Ax + 8 = 0 → Ax = −8 kN
ΣFy = Ay = 0 (no vertical applied load)
ΣMA = 0: (8 kN)(3 m) − (unknown moment at BC or internal reactions) = 0
Actually, it's clearer to dismember and apply local equilibrium.
Step 3: Dismember at joint C.
At C, three forces meet:
- Force FAC along AC (from A to C, or C to A)
- Force FBC along BC (vertical)
- Applied load of 8 kN (horizontal)
Force along AC: The member AC has components Δx = 4, Δy = 3, length 5.
Unit vector from A to C: (4/5, 3/5) = (0.8, 0.6)
If FAC is tension (pulling at C toward A), its components are:
FAC × (−0.8, −0.6) = (−0.8 FAC, −0.6 FAC)
Force along BC: FBC acts vertically (either up or down).
Step 4: Joint equilibrium at C.
ΣFx at C: −0.8 FAC + 8 = 0 → FAC = 10 kN (tension)
ΣFy at C: −0.6 FAC + FBC = 0 → FBC = 0.6(10) = 6 kN (compression, pushing upward on member BC)
Verification: The forces are consistent with a load pulling to the right—AC is pulled into tension, BC is compressed.
Answer: FAC = 10 kN (tension), FBC = 6 kN (compression).
Key points
- Frames contain at least one multi-force member, distinguishing them from trusses
- Multi-force members develop shear, bending moment, and axial force
- Analysis requires dismembering the frame and applying equilibrium to each member separately
- Two-force members carry force along their axis only—identify these first to reduce unknowns
- Newton's third law governs pin forces: equal magnitude, opposite direction on connected members
- External reactions are found first by treating the entire frame as a single free body
- Pin forces are internal forces and do not appear in the external equilibrium equation
2. Machines: Mechanical Advantage and Force Transmission
A machine is a structure or mechanism designed to transmit or modify forces and displacements. Unlike frames, which are typically stationary, machines often contain moving parts such as linkages, levers, pulleys, and ratchets. Examples include pliers, hydraulic jacks, hand-operated clamps, and mechanical advantage devices used on construction sites.
Fundamental Principle:
Machines operate on the principle of work: a small effort applied over a large distance may produce a large load over a small distance. The mechanical advantage (M.A.) is the ratio of output force (load) to input force (effort):
M.A. = Load / Effort = Effort Arm / Load Arm (for a simple lever)
Analysis Method:
Machines are analyzed exactly like frames—by dismembering and applying equilibrium to each member. However, the objective differs: instead of finding internal forces, we find the relationship between the effort (applied force) and the load (resistive force).
Simple Lever:
A lever pivots about a fulcrum. For a lever in equilibrium:
ΣM_fulcrum = 0:
Effort × Effort Arm = Load × Load Arm
M.A. = Load / Effort = Effort Arm / Load Arm
For ideal (frictionless) levers, M.A. > 1 means the lever amplifies force (but the effort moves farther than the load). M.A. < 1 means the lever amplifies displacement (useful for reaching or applying force over distance).
Compound Machines:
When multiple machines are combined (e.g., two levers in sequence), the overall M.A. is the product of individual advantages. However, real machines always lose energy to friction, so the actual M.A. is less than the theoretical value. The efficiency η is:
η = Actual M.A. / Theoretical M.A.
Practical Considerations for Civil Engineers:
In construction equipment analysis (cranes, winches, jacks), the mechanical advantage of the system determines how much load can be lifted or moved with a given effort. This is critical in design calculations per ASME standards and safe working load determinations.
Examples
A simple lever jack used on construction sites has a lever arm of 0.8 m from the fulcrum to the effort point and 0.10 m from the fulcrum to the load (a car). If the maximum effort a worker can apply is 300 N, what is the maximum load (weight) that can be lifted? Assume an ideal (frictionless) lever.
Answer
2400 N (2.4 kN)
Solution
Given:
Effort Arm = 0.8 m
Load Arm = 0.10 m
Effort = 300 N
Calculation:
Mechanical Advantage (M.A.) = Effort Arm / Load Arm = 0.8 / 0.10 = 8
For equilibrium of the lever:
Effort × Effort Arm = Load × Load Arm
Load = Effort × (Effort Arm / Load Arm) = 300 N × 8 = 2400 N
Alternatively:
Load = Effort × M.A. = 300 × 8 = 2400 N = 2.4 kN
Physical Interpretation:
The worker applies 300 N of force over a distance of 0.8 m, moving the load (2400 N) over a distance of 0.1 m. The work done by effort (300 × 0.8 = 240 J) equals the work done on the load (2400 × 0.1 = 240 J) in an ideal system.
Answer: Maximum load = 2400 N or 2.4 kN.
A pair of pliers has a handle length of 0.15 m from pivot to grip (effort arm) and a jaw length of 0.03 m from pivot to the object being gripped (load arm). (a) Calculate the ideal M.A. (b) If friction and material deformation reduce the actual M.A. to 85% of the ideal, what gripping force results from a 150 N hand squeeze?
Solution
Given:
Effort Arm = 0.15 m
Load Arm = 0.03 m
Effort = 150 N
Efficiency η = 0.85
(a) Ideal Mechanical Advantage:
M.A._ideal = Effort Arm / Load Arm = 0.15 / 0.03 = 5
(b) Actual Gripping Force:
M.A._actual = η × M.A._ideal = 0.85 × 5 = 4.25
Gripping Force = Effort × M.A._actual = 150 N × 4.25 = 637.5 N
Discussion:
Without the 85% efficiency factor (perfect conditions), the gripping force would be 150 × 5 = 750 N. Real pliers lose about 12.5% of theoretical advantage due to friction at the pivot and slight bending of the jaws.
Answer: (a) Ideal M.A. = 5. (b) Actual gripping force = 637.5 N.
A differential pulley system on a construction site uses two diameters: the large pulley has a diameter of 0.4 m, and the small pulley has a diameter of 0.35 m. When the effort rope is pulled, it unwinds from the large pulley and winds onto the small pulley in one revolution. Determine the M.A. and the load that can be lifted with a 400 N effort.
Solution
Concept:
In a differential pulley (also called a chain hoist), the effort rope unwinds from a large pulley of radius R_L and winds onto a smaller pulley of radius R_S. In one rotation, the load is lifted by the difference in circumferences.
Given:
Diameter_L = 0.4 m → Radius_L = 0.2 m
Diameter_S = 0.35 m → Radius_S = 0.175 m
Effort = 400 N
Calculation:
In one complete revolution:
- Rope unwound from large pulley: 2πR_L = 2π(0.2) = 0.4π m
- Rope wound onto small pulley: 2πR_S = 2π(0.175) = 0.35π m
- Net rope released (lifting load): 0.4π − 0.35π = 0.05π m
M.A. = Circumference_L / (Circumference_L − Circumference_S) = 2πR_L / [2π(R_L − R_S)]
M.A. = R_L / (R_L − R_S) = 0.2 / (0.2 − 0.175) = 0.2 / 0.025 = 8
Load = Effort × M.A. = 400 N × 8 = 3200 N = 3.2 kN
Answer: M.A. = 8; Load lifted = 3200 N (3.2 kN).
Key points
- Machines transmit and modify forces using mechanical advantage (M.A.)
- M.A. = Load / Effort = Effort Arm / Load Arm for simple levers
- Analysis uses the same dismembering and equilibrium methods as frames
- Moment equilibrium about the pivot is the key equation: Effort × Effort Arm = Load × Load Arm
- Ideal machines have M.A. = Effort Arm / Load Arm; real machines include friction losses (efficiency < 100%)
- Compound machines multiply individual advantages: overall M.A. = M.A.₁ × M.A.₂ × ... (ideally)
- For safety, actual (working) mechanical advantage accounts for friction and is always less than theoretical
- Civil applications include hand jacks, come-alongs, differential pulleys, and hydraulic systems
3. Cables: Tension, Shape, and Load Analysis
A cable is a perfectly flexible structural member that can sustain only tension (no compression or bending). Its shape is determined entirely by the loading applied to it. Cables are fundamental in suspension bridges, guy-wires for towers, and sag vertical takeoff systems. Understanding cable behavior is essential for the PRC examination, particularly in problems involving suspension structures and cable-stayed systems.
Fundamental Property:
At any point along a cable, the internal force is tangent to the cable and acts in tension only. If the cable makes an angle θ with the horizontal at a point, the tension T at that point has components:
- Horizontal: T cos(θ)
- Vertical: T sin(θ)
Critical Insight: Constant Horizontal Component
For a cable in equilibrium under any loading pattern, the horizontal component of tension H is constant throughout the cable. This is a consequence of horizontal force equilibrium—if H varied, there would be a net horizontal force on the system, violating equilibrium.
This property is the key to solving cable problems: once you find H, you can find the tension T at any point using T = H / cos(θ).
Cable Under Concentrated Loads:
When a cable supports discrete point loads, it forms a polygon (funicular polygon). Between loads, the cable is straight (no distributed load along the segment). The shape is determined by the magnitudes and positions of the loads.
Analysis at a Point Load:
At a point where a concentrated load P acts downward, the cable bends, and the two segments meeting at that point make different angles with the horizontal. Vertical force equilibrium at that point gives:
T₁ sin(θ₁) + T₂ sin(θ₂) = P
where T₁ and T₂ are the tensions in the two segments and θ₁, θ₂ are their angles.
Since H is constant:
T₁ cos(θ₁) = T₂ cos(θ₂) = H
Cable Under Uniform Horizontal Load (Parabolic Cable):
When a cable supports a load uniformly distributed over the horizontal span (typical of suspension bridge decks), the cable forms a parabola. For such cables:
- Span: L
- Sag (maximum deflection at midspan): d
- Uniform load per unit horizontal distance: w
The horizontal component of tension:
H = wL² / (8d)
The maximum tension occurs at the supports (steepest point):
T_max = √[H² + (wL/2)²]
where (wL/2) is the vertical reaction at a support.
Cable Under Self-Weight (Catenary):
When the cable's own weight is significant relative to external loads (or is the primary load), the shape is a catenary (the curve of a hanging chain). The shape is given by the hyperbolic cosine function:
y = (H/w) × cosh(wx/H)
For shallow sags (d << L), the parabola is a good approximation to the catenary. However, for deep sags or where self-weight dominates, the catenary must be used. The catenary has no simple closed-form relationship for tension; numerical methods are often required.
Practical Distinction:
- Parabolic: Load applied horizontally (e.g., suspension bridge deck per meter of span)
- Catenary: Load applied along the cable length (e.g., cable's own weight)
Design Considerations per Philippine Standards:
When designing cable systems in the Philippines (e.g., guyed towers, suspension structures), engineers must account for:
- Permanent loads (self-weight of cable, deck)
- Live loads (traffic, wind, seismic per NSCP 2015)
- Temperature effects (expansion and contraction)
- Environmental factors (corrosion, UV for exposed cables)
- Safety factors per ASME B30 and relevant codes
Examples
A suspension bridge has a main span of 40 m with a cable sag of 4 m at midspan. The cable supports a uniformly distributed load of 6 kN/m of horizontal span (representing the weight of the deck and traffic). Determine: (a) the horizontal component of cable tension H, (b) the maximum cable tension (at the supports), (c) the cable length if we approximate the parabolic cable.
Answer
(a) H = 300 kN. (b) T_max = 323.1 kN. (c) S ≈ 41.1 m.
Solution
Given:
Span L = 40 m
Sag d = 4 m
Uniform load w = 6 kN/m (horizontal)
(a) Horizontal component of tension:
For a parabolic cable under uniform horizontal load:
H = wL² / (8d)
H = 6 × 40² / (8 × 4)
H = 6 × 1600 / 32
H = 9600 / 32
H = 300 kN
(b) Maximum cable tension:
The maximum tension occurs at the supports where the cable is steepest. At midspan, the cable is horizontal (slope = 0). At the supports, the slope is maximum.
For a parabolic cable, the slope at position x from midspan is:
dy/dx = (8d/L²) × x
At the support (x = L/2 = 20 m):
dy/dx = (8 × 4 / 40²) × 20 = (32 / 1600) × 20 = 0.02 × 20 = 0.4
Slope angle: tan(θ) = 0.4 → θ = arctan(0.4) = 21.80°
sin(θ) = 0.3714, cos(θ) = 0.9285
At the support, the vertical component of tension equals the total vertical reaction, which is half the total load:
V = wL/2 = 6 × 40 / 2 = 120 kN
The tension at the support:
T_max = √(H² + V²) = √(300² + 120²) = √(90000 + 14400) = √104400 = 323.1 kN
Alternatively:
T_max = H / cos(θ) = 300 / 0.9285 = 323.1 kN ✓
(c) Cable length (parabolic approximation):
For a parabola y = (8d/L²)x² (with origin at midspan and x ranging from −L/2 to +L/2):
The arc length is approximated by:
S ≈ L[1 + (8/3)(d/L)²] for small sag-to-span ratios
With d/L = 4/40 = 0.1:
S ≈ 40[1 + (8/3)(0.1)²]
S ≈ 40[1 + (8/3)(0.01)]
S ≈ 40[1 + 0.0267]
S ≈ 40 × 1.0267
S ≈ 41.07 m
More precisely, the parabolic arc length from x = −20 to x = +20 with y = (8 × 4 / 1600)x² = 0.02x²:
ds = √(1 + (dy/dx)²) dx = √(1 + (0.04x)²) dx
Integrating numerically or using the formula above:
S ≈ 41.1 m
Answer: (a) H = 300 kN. (b) T_max = 323.1 kN. (c) Cable length ≈ 41.1 m.
Key points
- Cables carry tension only; no compression or bending moments
- Cable shape is determined by the loading pattern applied to it
- The horizontal component of tension H is constant throughout the cable—this is the key to cable analysis
- Tension at any point T = H / cos(θ), where θ is the angle of the cable at that point
- Concentrated loads create a funicular polygon (straight segments between loads)
- Uniform horizontal load creates a parabolic cable shape
- For parabolic cables: H = wL² / (8d), where w is load per unit horizontal distance, L is span, d is sag
- Maximum tension in a parabolic cable occurs at the supports: T_max = √[H² + (wL/2)²]
- Self-weight of the cable creates a catenary shape, not a parabola
- For shallow sags, the parabola approximates the catenary sufficiently for design
- Cable tension increases as the cable slope increases (steeper sections have higher tension)
4. Comparison: Trusses vs. Frames vs. Machines vs. Cables
To consolidate understanding, this section compares the four primary structural systems encountered in engineering mechanics.
Trusses:
- Definition: Structure composed entirely of two-force members (loaded only at their ends).
- Internal forces: Axial only (tension or compression); no shear or bending.
- Analysis methods: Method of joints (equilibrium at each joint) or method of sections (cut and analyze portions).
- Common use: Roof trusses, bridge trusses, lattice towers.
- Advantage: Efficient for long spans with minimal deflection; simple force distribution.
- Limitation: Cannot easily carry transverse loads on members.
Frames:
- Definition: Stationary structures containing at least one multi-force member.
- Internal forces: Axial, shear, and bending moment all may be present.
- Analysis method: Dismembering (separate into individual members and apply equilibrium to each).
- Common use: Building frames, brackets, portal frames.
- Advantage: Can support transverse loads and moments; flexible design.
- Limitation: More complex analysis; greater deflections under load.
Machines:
- Definition: Mechanisms designed to transmit or modify forces; often contain moving parts.
- Internal forces: Same as frames (axial, shear, bending), but focus is on force multiplication (mechanical advantage).
- Analysis method: Dismembering plus calculation of M.A. = Load / Effort.
- Common use: Pliers, jacks, pulleys, levers, winches.
- Advantage: Amplify applied force to move/lift larger loads.
- Limitation: Mechanical advantage decreases with friction and deformation.
Cables:
- Definition: Perfectly flexible members carrying tension only; shape determined by loading.
- Internal forces: Tension (no compression, shear, or bending).
- Key property: Horizontal component of tension is constant throughout.
- Analysis method: Identify shape (funicular polygon for concentrated loads, parabola for uniform horizontal load, catenary for self-weight); apply equilibrium at each load point or use integration.
- Common use: Suspension bridges, guy-wires, roof support systems.
- Advantage: Extremely efficient for long spans; minimal material needed.
- Limitation: Sensitive to load distribution; cannot carry compression; large deflections under live load.
Comparison Table:
| Property | Truss | Frame | Machine | Cable |
|---|---|---|---|---|
| Member Types | Two-force only | Multi-force | Multi-force (moving) | Flexible tension |
| Loads | At joints | On members | On members | Distributed or concentrated |
| Internal Forces | Axial only | Axial, shear, bending | Axial, shear, bending | Tension only |
| Shape | Fixed | Fixed | Fixed | Variable (load-dependent) |
| Analysis | Joints or sections | Dismember | Dismember + M.A. | Equilibrium + geometry |
| Efficiency | High | Moderate | Variable | Very high (span/material) |
| Deflection | Small | Moderate | Depends on load | Large (sag) |
Decision Tree for Analysis:
When presented with a structural system:
- Is the structure entirely composed of two-force members? → Truss (use method of joints or sections)
Are there multi-force members?
- Stationary structure? → Frame (dismember and apply equilibrium)
- Designed to transmit forces or move? → Machine (dismember + find mechanical advantage)
- Is the member flexible and carries only tension? → Cable (identify shape and apply equilibrium)
This systematic approach ensures correct identification and appropriate analysis method.
Key points
- Trusses have two-force members only; frames and machines have multi-force members
- Frames are stationary; machines are designed to transmit or modify forces
- Cables are flexible and carry tension only; their shape depends on the loading
- Analysis methods differ: trusses use joints/sections, frames/machines use dismembering, cables use equilibrium + geometry
- Mechanical advantage (M.A.) is the defining characteristic of machines
- The constant horizontal component of tension simplifies cable analysis
- Choice of analysis method depends on the structure type and the nature of internal forces
- Efficiency (span-to-material ratio) varies: cables are most efficient, trusses are next, frames are less efficient
- Deflections increase as flexibility increases: cables deflect most, trusses least
5. Common Board-Exam Mistakes and Problem-Solving Tips
Success on the PRC Civil Engineer Licensure Examination requires not only understanding concepts but also avoiding common pitfalls and applying strategic problem-solving approaches.
Common Mistakes:
Treating a Frame Member as Two-Force When It Carries a Transverse Load
- Mistake: Assuming a member carrying a mid-span load is a two-force member and directing its internal force along the member axis.
- Correction: Multi-force members develop shear and bending. Always apply full equilibrium (ΣFx, ΣFy, ΣM) to each dismembered member, not just force balance along the member axis.
- Exam implication: A 15 kN load applied mid-span on a beam makes it multi-force, not two-force, even if it appears to be a "strut".
Forgetting Newton's Third Law at Pins
- Mistake: Assigning the same direction to pin forces on both members sharing a pin.
- Correction: At every pin, the force exerted by member A on member B is equal in magnitude but opposite in direction to the force exerted by B on A.
- Exam implication: If your FBDs don't satisfy action-reaction pairs at shared pins, recalculate immediately.
- Check: On the beam's FBD, if the strut pushes upward at the pin, on the strut's FBD, the beam must push downward at the same pin.
Mixing Up Load Arm and Effort Arm in M.A. Calculations
- Mistake: Using M.A. = Load Arm / Effort Arm (inverted).
- Correction: M.A. = Effort Arm / Load Arm. The longer the effort arm, the greater the mechanical advantage.
- Exam implication: A lever with a 1.0 m effort arm and 0.1 m load arm has M.A. = 1.0 / 0.1 = 10, not 0.1.
- Memory aid: A longer effort arm multiplies the effort force.
Assuming Cable Horizontal Component H Changes Along the Cable
- Mistake: Solving for H at different points and getting different values (indicating an error in geometry or equilibrium).
- Correction: H is constant throughout the cable. If your calculations yield different H values at different points, recheck geometry, load application, or equilibrium equations.
- Exam implication: This is a powerful check—if H varies, your setup is wrong.
Confusing Parabolic (Uniform Horizontal Load) with Catenary (Self-Weight)
- Mistake: Using the parabolic formula H = wL² / (8d) for a cable whose primary load is its own weight.
- Correction: Self-weight (or load distributed along the cable length) creates a catenary, not a parabola. The catenary formula is more complex and often requires numerical methods.
- Exam implication: The problem statement will indicate whether the load is "distributed horizontally" (parabola) or "distributed along the cable length" (catenary). Read carefully.
- Rule of thumb: Suspension bridge decks (uniform horizontal load) → parabola. Power transmission lines (self-weight) → catenary.
Finding Tension at the Wrong Location
- Mistake: Calculating the maximum tension at midspan when it actually occurs at the support (steepest slope).
- Correction: Cable tension is maximum where the slope is steepest. For a hanging cable, the steepest point is always at or near the supports, never at midspan (where the cable is often horizontal).
- Exam implication: T_max = √(H² + V²) or T_max = H / cos(θ_max), where θ_max occurs at the support.
Not Identifying Two-Force Members Before Dismembering
- Mistake: Treating all members equally when dismembering, resulting in unnecessary unknowns.
- Correction: Before applying equilibrium, identify which members are two-force members. For these, the force direction is known (along the member), reducing unknowns by one.
- Exam implication: A frame with 4 members, 2 of which are two-force, has 2 fewer unknowns than if all were multi-force. This saves calculation time.
- Quick check: If a member is pinned at both ends and has no intermediate loads or moments, it's two-force.
Forgetting Support Reactions When Dismembering
- Mistake: Neglecting the support reactions (from the wall, ground, or fixed support) when drawing the FBD of an individual member.
- Correction: When dismembering, include all forces acting on each member: applied loads, pin forces from connected members, and reactions from supports attached to that member.
- Exam implication: If the frame is pinned to a wall at point A, the wall reaction must appear on the FBD of the member connected to the wall.
Applying Moment Equilibrium About the Wrong Point
- Mistake: Using ΣM = 0 about a point when it's mathematically valid but not strategically helpful (results in complicated algebra).
- Correction: Choose moment reference points strategically—usually at a point where unknown forces pass through (making them "disappear" from the moment equation).
- Exam implication: If trying to find a pin force and you have two unknowns, take moments about the other unknown's location; the resulting moment equation contains only one unknown.
Ignoring Geometry in Cable Problems
- Mistake: Not clearly defining the angles (slopes) of cable segments relative to the horizontal.
- Correction: Always draw the cable geometry carefully, label all angles, and use sin(θ) = (vertical distance) / (segment length), cos(θ) = (horizontal distance) / (segment length).
- Exam implication: Geometry errors cascade through cable calculations. A 2° error in θ can yield 5%+ error in T.
Strategic Problem-Solving Tips:
Draw Large, Clear Free-Body Diagrams (FBDs)
- A large FBD is your best defense against sign errors and missed forces.
- Include all forces: applied loads, pin forces, support reactions, and any distributed loads.
- Label every force with a symbol and assumed direction (you can correct the sign later).
Use Consistent Sign Convention
- Choose one consistently: e.g., rightward = +x, upward = +y, counterclockwise = +M.
- Stick to it throughout the problem. When writing ΣF or ΣM equations, substitute forces and moments with their algebraic signs.
Write Equilibrium Equations Algebraically, Not Component-by-Component
- Instead of "Horizontal forces: rightward = leftward", write "ΣFx = 0: 24 − Ax = 0".
- This avoids the pitfall of balancing directions intuitively rather than algebraically.
Solve Systems of Equations Systematically
- If you have 3 unknowns (e.g., Ax, Ay, Fs), write 3 independent equations.
- Use substitution or elimination; don't rely on intuition or trial-and-error.
- For the board exam, show your algebra: partial credit is awarded for correct approach even if the final number is wrong.
Check Your Answer by Substitution or an Independent Method
- After finding Fs = 33.9 kN, substitute it back into one of the original equations to verify.
- If using a different method (e.g., moment about a different point), the answer should match.
For Cable Problems, Always Verify That H Is Constant
- Calculate H at different points (different load points or supports).
- If H differs, there's an error. Recheck geometry or equilibrium.
Estimate Before Calculating
- For a 12 m span with a 1.5 m sag and a 10 kN central load, estimate H ≈ (10 × 6 m) / 1.5 m ≈ 40 kN (very rough).
- Your detailed calculation should be in the same ballpark. If it's wildly different, recheck.
Unit Consistency
- Use SI units throughout: kN for forces, m for distances, kN/m for distributed loads.
- If given mixed units (kips, feet), convert immediately at the start.
Margin of Safety and Realistic Values
- In practice, cable tensions are often 2–3× the minimum theoretical value (for safety and fatigue).
- A calculated tension that's physically unreasonable (e.g., 100 MPa for a typical structural cable) suggests an error.
Practice with Real Examples
- Study actual bridge cable analyses, building frame designs, and machine sketches from civil engineering references.
- The PRC exam often uses real-world scenarios; familiarity with practical systems aids intuition.
Key points
- Verify that each member's FBD is consistent with Newton's third law at pins
- Identify two-force members early to simplify the analysis
- Use strategic moment equilibrium about points that eliminate unknowns
- Verify that the horizontal component of cable tension is constant (not varying)
- Distinguish between parabolic (uniform horizontal load) and catenary (self-weight) shapes
- Maximum cable tension occurs at the steepest slope, typically at the supports
- Draw large, labeled FBDs for every member
- Use algebraic equilibrium equations with consistent sign convention
- Check answers by substitution or independent calculation
- Estimate rough values before detailed calculation to catch major errors
Diagrams
Frames, Machines, and Cables: Structural Systems Overview
This mind map organizes the four primary structural systems encountered in engineering mechanics, highlighting their distinguishing features and analysis methods. Trusses appear for reference; the chapter focuses on frames, machines, and cables.
Frame and Machine Analysis: Dismembering Method
This flowchart outlines the systematic process for analyzing frames and machines using the dismembering method. Key steps include identifying two-force members, finding external reactions, dismembering the structure, applying equilibrium to each member, and verifying consistency using Newton's third law.
Cable Shape and Analysis Selection
This decision flowchart guides the analyst in selecting the appropriate cable model based on the type of loading. It emphasizes the key formula for parabolic cables and the constant horizontal tension property that applies to all cable configurations.
Problem-Solving State: From Problem to Verified Solution
This state diagram illustrates the problem-solving workflow for frames, machines, and cables, emphasizing the importance of verification steps: substitution checks, constant horizontal tension in cables, Newton's third law confirmation, and comparison to rough estimates.
In summary
Frames, Machines, and Cables represent three fundamental structural systems in engineering mechanics, each with distinct characteristics and analysis methods.
Frames are stationary structures containing multi-force members that develop axial force, shear, and bending. Analysis requires dismembering the frame into individual members and applying equilibrium equations (ΣFx = 0, ΣFy = 0, ΣM = 0) to each member. Newton's third law governs pin forces—equal magnitude, opposite direction at shared pins. Two-force members, identified early, simplify the analysis by reducing unknowns.
Machines are similar to frames but designed to transmit or modify forces. The key output is the mechanical advantage (M.A. = Load / Effort = Effort Arm / Load Arm for simple levers). Analysis uses the same dismembering approach as frames, with the added calculation of force multiplication. Real machines incur friction losses; the actual M.A. is the theoretical M.A. multiplied by efficiency (η < 100%).
Cables are perfectly flexible members carrying tension only. Their shape is dictated by the loading: concentrated loads create a funicular polygon; uniform horizontal load creates a parabola; self-weight creates a catenary. The critical property is that the horizontal component of tension H is constant throughout the cable. For parabolic cables under uniform load, H = wL² / (8d), and maximum tension (at supports) is T_max = √(H² + (wL/2)²). Cable analysis relies on geometry (slope angles) and equilibrium at load points or supports.
Comparison: Trusses contain two-force members only and are analyzed by joints or sections. Frames have multi-force members and are analyzed by dismembering. Machines are like frames but emphasize force transmission. Cables are flexible and shape-shifting, analyzed through geometry and equilibrium. Efficiency (span-to-material ratio) is highest for cables, next for trusses, and lower for frames.
Common Board-Exam Pitfalls: (1) Treating multi-force members as two-force. (2) Forgetting Newton's third law at pins. (3) Inverting the M.A. formula. (4) Assuming H varies along a cable. (5) Confusing parabolic with catenary shapes. (6) Finding maximum tension at the wrong location. (7) Neglecting to identify two-force members early. (8) Missing support reactions in FBDs. (9) Using non-strategic moment equilibrium points. (10) Poor geometry in cable problems.
Success Strategy: Draw large, clear FBDs with all forces labeled. Use consistent sign conventions. Write equilibrium equations algebraically. Identify two-force members and use strategic moment equilibrium. Verify H is constant in cables. Check answers by substitution. Estimate rough values before detailed calculation. With practice and attention to these methods, frames, machines, and cables become straightforward applications of equilibrium and geometry—core competencies for the PRC Civil Engineer Licensure Examination.