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CELE Structural Theory & AnalysisAnalysis of Determinate StructuresStudy Notes

Complete study notes for Analysis of Determinate Structures, written for CELE aspirants. Unlike generic notes, these focus on what Professional Regulation Commission (PRC) — Board of Civil Engineering actually tests in the CELE Structural Theory & Analysis section: high-yield concepts, common question types, and the worked examples that match recent exam patterns.

Exam context

On the CELE 2026, the Structural Theory & Analysis subtest carries a "Core" weight in Professional Regulation Commission (PRC) — Board of Civil Engineering's pattern. Analysis of Determinate Structures lands at position 1st out of 6 in the standard review order. Target score is 70% weighted average, no sub-test below 50%, and roughly a meaningful share of items come from Structural Theory & Analysis on a typical CELE paper.

Analysis of Determinate Structures - Study Notes

Structural analysis is the fundamental skill that allows engineers to understand how buildings, bridges, and other structures respond to loads. The first critical decision in any analysis is determining whether a structure is statically determinate—solvable using equilibrium equations alone—or statically indeterminate, requiring additional compatibility equations. This chapter covers the essential concepts of determinacy and stability, methods for finding reactions in determinate structures, calculation of internal forces (axial, shear, and moment), and special cases like three-hinged arches and compound (Gerber) beams. Mastering these concepts is essential for the PRC Civil Engineer Licensure Examination and forms the foundation for advanced structural analysis, design of reinforced concrete per ACI 318, and steel design per AISC 360-16.

Summary

Analysis of determinate structures is the foundation of structural engineering, providing engineers with the ability to find reactions, internal forces, and stresses in structures solvable by equilibrium alone. This chapter covered the critical distinction between static determinacy (enough equations to solve from equilibrium) and stability (proper arrangement of reactions to resist all loads). Key topics include: (1) determinacy classification using DI = (3m + r) - (3n + e_c), (2) the role of internal hinges as equations of condition, (3) systematic analysis of reactions using free body diagrams and equilibrium equations, (4) calculation and diagramming of internal forces (axial, shear, and moment), (5) special determinate structures like three-hinged arches (which use horizontal thrust to reduce moments), and (6) compound (Gerber) beams that strategically use internal hinges to achieve determinacy. Frame analysis extends these concepts to rigid structures with multiple members and moment continuity at joints. Throughout this chapter, proper sign conventions, careful free body diagrams, and systematic verification of results are emphasized as essential skills to avoid common analysis errors. Mastery of determinate structure analysis is required before proceeding to indeterminate structures and is directly applicable to design per ACI 318 (reinforced concrete), AISC 360 (steel), and NSCP 2015 (Philippine building code). These skills are essential for success on the PRC Civil Engineer Licensure Examination and for competent professional practice in structural engineering and design.

Sections

The concept of static determinacy is central to structural analysis. A structure is statically determinate if all reaction components and internal forces can be found using only the three fundamental equilibrium equations: ΣFx = 0, ΣFy = 0, and ΣM = 0. If additional equations are needed—such as compatibility of deformation—the structure is statically indeterminate. To classify a structure's determinacy, we count the number of unknown reaction components (r) and compare them against the number of independent equilibrium equations available (3 for planar structures, 6 for spatial structures). For planar structures, the degree of static indeterminacy (DI) is expressed as: DI = (3m + r) - (3n + e_c) Where: - m = number of members - r = number of reaction components - n = number of joints (nodes) - e_c = number of equations of condition (internal releases) Alternatively, for simple beams and cantilevered structures: DI = r - (3 + e_c) The interpretation is straightforward: - DI = 0: Statically determinate (solvable by equilibrium alone) - DI > 0: Statically indeterminate to degree DI (requires DI additional equations) - DI < 0: Statically unstable (too few reactions or improper arrangement) Each internal hinge or pin connection between members acts as an equation of condition. A single internal hinge adds one equation of condition, corresponding to the moment equilibrium equation at that hinge (ΣM_hinge = 0 on either side). Understanding determinacy is crucial because it tells the engineer which analysis method to use. For determinate structures, classical methods (method of sections, method of joints) are efficient. For indeterminate structures, more advanced techniques like slope-deflection, moment distribution, or matrix methods are required. In the context of Philippine building design per NSCP 2015 (National Structural Code of the Philippines), all structures must be analyzed to ensure both determinacy and stability before proceeding to design. Improper structural configurations leading to instability or hidden indeterminacy can result in design failures.

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1. Fundamental Concepts: Determinacy vs. Indeterminacy

Examples

Example 1.1: Simple Supported Beam with Overhang

A simple supported beam with one overhang has three reaction components (two at the simple support, one at the cantilever support = 3 reactions total). Using DI = r - (3 + e_c) = 3 - 3 = 0. This structure is statically determinate.

Calculation

For a simple beam: r = 3 (one vertical and one horizontal at one support, one vertical at the other). Since there are exactly 3 equations of equilibrium and no internal releases, DI = 0. All reactions can be found from ΣFx = 0, ΣFy = 0, ΣM = 0.

Example 1.2: Portal Frame with Fixed Bases

A portal frame with fixed bases (typical industrial building) has m = 3 (two columns and one beam), r = 6 (three reactions per fixed base: vertical, horizontal, moment), n = 4 (four joints: two bases and two top corners), e_c = 0 (no internal hinges).

Calculation

DI = (3m + r) - (3n + e_c) = (3×3 + 6) - (3×4 + 0) = 15 - 12 = 3. This frame is statically indeterminate to the 3rd degree. Three additional equations (from compatibility) are needed to solve completely. This is typical for portal frames and requires moment distribution or slope-deflection methods.

Example 1.3: Gerber Beam (Compound Beam) with Internal Hinge

A continuous beam of 20 m total length (two 10 m spans) with an internal hinge (pin) at midspan creates an equation of condition. r = 4 (two reactions at left support, two at right support), e_c = 1 (one internal hinge).

Calculation

DI = r - (3 + e_c) = 4 - (3 + 1) = 0. The internal hinge is strategically used to make the structure determinate. The hinge means that the bending moment at that point must be zero, providing one additional equation: ΣM_hinge = 0.

Key Points

  • Static determinacy is determined by comparing number of unknowns (reactions) with available equilibrium equations
  • Formula for planar structures: DI = (3m + r) - (3n + e_c) or simplified DI = r - (3 + e_c) for beams
  • Internal hinges and pins add equations of condition (e_c) and reduce indeterminacy
  • DI = 0 indicates determinate structure; DI > 0 indicates indeterminate; DI < 0 indicates unstable
  • Determinacy classification must precede selection of analysis method
  • NSCP 2015 and ACI 318 require verification of structural stability and determinacy

It is absolutely essential to understand that static determinacy and structural stability are two separate considerations. A structure can be statically determinate yet unstable, or vice versa. Stability refers to whether the structure can resist movement in all directions. A structure is unstable if: 1. The reaction components are concurrent (all lines of action pass through a single point)—the structure can rotate about that point. 2. The reaction components are parallel (all lines of action are parallel)—the structure can translate perpendicular to them. 3. There are fewer than 3 linearly independent reaction components in planar structures. 4. The arrangement provides no resistance to a particular direction of loading. Consider a simple example: A cantilever beam has 3 reaction components (one moment, one vertical, one horizontal at the fixed end), so DI = 3 - 3 = 0 (determinate). However, if the support is incorrectly designed such that it cannot provide horizontal resistance, the structure becomes unstable despite being determinate on paper. In the context of NSCP 2015, structural design must ensure that: 1. The structure is stable under all potential loading conditions. 2. Load paths are clear and continuous to the foundation. 3. Lateral stability (especially for tall structures) is verified per NSCP 2015 Chapter 4. For buildings designed per ACI 318 (reinforced concrete), the structure must be capable of transmitting all loads (dead, live, seismic per NSCP 2015 Chapter 5) to the foundation safely. If any directional load path is missing, the structure fails regardless of determinacy classification. The key principle: Always verify that the structure can resist loads from all directions, not just count reaction components. Proper structural layout ensures both stability and appropriate determinacy for the intended design method.

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2. Stability vs. Determinacy: A Critical Distinction

Examples

Example 2.1: Determinate but Unstable Structure

A simple beam supported on two frictionless rollers (both providing vertical reactions only). The structure has r = 2 (both vertical), so by counting it appears determinate. However, there is no horizontal reaction component. If the beam experiences horizontal loads (wind, seismic, accidental impact), the structure is unstable.

Calculation

DI = 2 - 3 = -1, indicating instability. The negative DI correctly identifies the problem: insufficient reaction components.

Example 2.2: Three Concurrent Reactions

A triangular truss with three reaction components that all meet at a point (concurrent forces). Although r = 3, the structure can rotate about the point of concurrency without internal member forces developing.

Calculation

Although DI = 3 - 3 = 0 on paper, the concurrent nature of reactions means the structure is unstable to rotation. Verification of reaction arrangement is essential.

Example 2.3: Proper Stable Configuration

A standard portal frame: two fixed bases provide reactions in vertical and horizontal directions plus moments. Reaction components are not concurrent or parallel, ensuring stability in all directions.

Calculation

DI = 3 (indeterminate), but more importantly, the structure is stable. It can resist vertical loads (gravity), horizontal loads (wind, seismic), and moments. This is why portal frames are standard in NSCP 2015 buildings.

Key Points

  • Static determinacy and structural stability are independent considerations
  • A structure can be determinate but unstable (e.g., reactions concurrent or parallel)
  • Unstable structures cannot resist all loading directions despite having enough equations
  • Stability check requires verification of reaction arrangement and load path continuity
  • NSCP 2015 requires explicit verification of both stability and determinacy
  • Proper load path: loads → members → connections → reactions → foundation

Once a structure is classified as determinate, the next step is to find all reaction components using equilibrium equations. The process is systematic: Step 1: Draw a free body diagram (FBD) of the entire structure, showing all external loads and reaction components (unknowns). Step 2: Apply the three equilibrium equations: - ΣFx = 0 (sum of horizontal forces) - ΣFy = 0 (sum of vertical forces) - ΣM = 0 (sum of moments about any point) Step 3: Solve the system of equations for reaction components. Step 4: If the structure contains internal hinges (equations of condition), use these to set up additional equations. For each internal hinge, the bending moment on one side must equal zero: ΣM_hinge = 0. For determinate beams and frames, the method is straightforward: - Vertical loads create vertical reactions. - Horizontal loads create horizontal reactions. - Moments create moment reactions (at fixed supports). Choosing the right moment reference point significantly simplifies calculations. It is often advantageous to take moments about a point where multiple unknowns act (eliminating those unknowns from the moment equation). For compound structures (Gerber beams with internal hinges), analyze from the free (suspended) span backward. The suspended span's internal hinge is where ΣM = 0, providing one equation. Solve for reactions on the suspended span first, then use its reaction as a load on the main span. Common support types and their reactions (per NSCP 2015): - Pin/Hinge support: 2 reaction components (vertical and horizontal) - Roller support: 1 reaction component (perpendicular to surface) - Fixed/Clamped support: 3 reaction components (two force components and one moment) The sign convention is critical for clarity and correctness. Typically: - Upward vertical forces: positive - Rightward horizontal forces: positive - Counterclockwise moments: positive

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3. Support Reactions in Determinate Structures

Examples

Example 3.1: Simple Supported Beam with Concentrated Load

A 10 m long beam supports a 40 kN vertical load at 6 m from the left support. Find all reactions.

Calculation

Let A be the left support (pin, 2 reactions: Ax and Ay) and B be the right support (roller, 1 reaction: By). ΣFx = 0: Ax = 0 (no horizontal load) ΣM_A = 0: By(10) - 40(6) = 0 → By = 24 kN ΣFy = 0: Ay + 24 - 40 = 0 → Ay = 16 kN Verification: ΣM_B = 0: Ay(10) - 40(10-6) = 16(10) - 40(4) = 160 - 160 = 0 ✓

Example 3.2: Cantilever Beam with Distributed Load

A cantilever beam of 5 m fixed at one end carries a uniformly distributed load (UDL) of 8 kN/m. Find reactions at the fixed support.

Calculation

Total distributed load: W = 8 × 5 = 40 kN, acting at the centroid (2.5 m from the free end). ΣFy = 0: Ay - 40 = 0 → Ay = 40 kN (upward) ΣM_A = 0: -MA + 40(2.5) = 0 → MA = 100 kN·m (counterclockwise) No horizontal load, so Ax = 0. The fixed support provides one vertical reaction (40 kN) and one moment reaction (100 kN·m).

Example 3.3: Gerber Beam with Internal Hinge

A 15 m compound beam (two 7.5 m spans) with an internal hinge at midspan (7.5 m). A 60 kN concentrated load acts 5 m from the left support. Find all reactions.

Calculation

Step 1: Analyze the right suspended span (hinge at C to right support B). At the hinge: ΣM_C = 0 (right portion). If load is only in left span: Cy = 0, CB_y = 0 Step 2: Analyze left span (A to hinge C). ΣM_A = 0: Cy(7.5) - 60(5) = 0 → Cy = 40 kN ΣFy = 0: Ay - 60 + 40 = 0 → Ay = 20 kN Step 3: Right span reactions equal vertical force at hinge. By = Cy = 40 kN Ax = 0 Note: This demonstrates the efficiency of Gerber beams—internal hinges reduce moments and reactions by allowing the suspended span to 'float' freely.

Key Points

  • Support reactions are found using three equilibrium equations: ΣFx = 0, ΣFy = 0, ΣM = 0
  • Free body diagram (FBD) must clearly show all loads and reaction components
  • Choice of moment reference point simplifies calculations (choose points where unknowns act)
  • Internal hinges provide equations of condition: ΣM_hinge = 0
  • For compound beams, analyze suspended span first, then carry reaction to main span
  • Support types determine number of reaction components: pin (2), roller (1), fixed (3)
  • Consistent sign convention ensures correct solution and proper interpretation

Once reactions are found, the internal forces (axial force N, shear force V, and bending moment M) can be determined at any section along the structure. These internal forces are what the structural material must resist and are used for member design. Definitions: Axial Force (N): The internal force acting along the axis of the member. It represents tension (pulling apart) or compression (pushing together). Found by cutting the member and applying equilibrium to one side: sum all forces parallel to the member axis. Shear Force (V): The internal force acting perpendicular to the member axis. It represents the tendency of one part of the member to slide relative to the other. Found by cutting the member and summing all forces perpendicular to the axis on one side. Bending Moment (M): The internal moment resisting rotation of the member cross-section. It causes curvature and bending stress. Found by cutting the member and taking moments about the section on one side. The method is always the same: 1. Cut the member at the section of interest. 2. Draw a free body diagram (FBD) of one side of the cut. 3. Apply equilibrium equations to that FBD. 4. Solve for N, V, and M. Sign Conventions (Standard for structural analysis per NSCP 2015): For beams aligned horizontally: - Positive shear: tends to rotate the cut section clockwise (or causes right part to move down relative to left) - Positive moment: causes compression in top fiber (sagging in spans, hogging at supports) - Axial tension: positive; compression: negative For columns or vertical members: - Positive axial: tension - Negative axial: compression - Shear and moment signs follow similar conventions Shear Force and Bending Moment Diagrams (SFD and BMD): These diagrams plot V and M as functions of position along the member. They are essential for identifying critical sections where maximum stress occurs. Key relationships: dV/dx = -w (where w is the distributed load intensity) dM/dx = V These relationships help sketch diagrams quickly: - Where w = 0, V is constant and M has constant slope (linear) - Where w is uniform, V changes linearly and M is parabolic - At points of concentrated load, V has a sudden jump; M has a kink - At points of concentrated moment, M has a sudden jump - Where V = 0, M reaches maximum or minimum For reinforced concrete design per ACI 318 and steel design per AISC 360-16, the maximum moment determines the required flexural reinforcement (steel area), and the maximum shear determines the required shear reinforcement (stirrups or shear reinforcement). Frames (rigid structures with multiple members): Each member is analyzed separately, and internal forces are continuous across rigid joints but can have discontinuities at hinges. At a rigid joint, the moment at the end of one member equals the moment at the start of the adjacent member (internal equilibrium at the joint).

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4. Internal Forces: Axial, Shear, and Bending Moment

Examples

Example 4.1: Internal Forces in Simple Beam at Midspan

A 12 m simple beam carries a 50 kN concentrated load at midspan. Find N, V, and M at the center of the span.

Calculation

Reactions: Ay = 25 kN, By = 25 kN, Ax = 0 (no horizontal load). At midspan (x = 6 m), cut the beam and consider the left portion (0 to 6 m): Axial force N: ΣF_horizontal = 0 → N = 0 (no horizontal forces) Shear force V: ΣF_vertical = 0 → 25 - V = 0 → V = 25 kN (positive by convention) Bending moment M: ΣM = 0 about the section → M - 25(6) = 0 → M = 150 kN·m (sagging, positive) This is the maximum moment. For a 50 kN load at midspan, the center always has maximum moment.

Example 4.2: Shear and Moment Diagram for Cantilever

A 6 m cantilever beam (fixed at x = 0, free at x = 6) carries a uniformly distributed load of 10 kN/m. Sketch SFD and BMD; find V and M at x = 3 m.

Calculation

Total load: W = 10 × 6 = 60 kN. Reaction at fixed end: Ay = 60 kN, MA = 10 × 6 × 3 = 180 kN·m. At x = 3 m (cut and consider right portion from x = 3 to x = 6): Load on right portion: 10(6 - 3) = 30 kN Shear: V = 30 kN (upward on left side of cut, positive) Moment: M = 10(6-3)²/2 = 10(9)/2 = 45 kN·m (sagging from right perspective, so M = 45 kN·m positive) SFD: Linear from 0 to 60 kN (increases from free end to fixed end, opposite of typical spans) BMD: Parabolic, maximum at fixed end (180 kN·m), zero at free end

Example 4.3: Internal Forces in Portal Frame Member

An L-shaped frame: vertical column AB (height 4 m, fixed at A, pin at B to horizontal member), horizontal beam BC (length 3 m, free at C). A 20 kN horizontal force acts at C (free end), 1 m above point B. Find reactions and internal forces at the column base.

Calculation

Reactions at fixed base A: Horizontal: Ax = 20 kN (reaction to applied load) Vertical: Ay = 0 (no vertical load) Moment: MA = 20 × (4 + 1) = 20 × 5 = 100 kN·m (the load is 1 m above B, and B is 4 m above A, but moment arm is from applied force location) Actually, recalculate: At B (height 4 m), the applied load creates moment = 20(1) = 20 kN·m. At base A, adding the column's own bending, total moment = 20 + 20(4) = 20 + 80 = 100 kN·m. Internal forces at column base (just above A): Axial: N = 0 Shear: V = 20 kN (horizontal frame member pushes on column) Moment: M = 100 kN·m Note: In frames, internal forces are typically resolved in member local coordinates for design.

Key Points

  • Axial force N: acts along member axis; found from ΣF_parallel = 0
  • Shear force V: acts perpendicular to member axis; found from ΣF_perpendicular = 0
  • Bending moment M: internal moment; found from ΣM = 0 about the section
  • Method: cut member → draw FBD of one side → apply equilibrium
  • Standard sign convention: positive shear tends to rotate section clockwise; positive moment causes compression in top fiber
  • Relationships: dV/dx = -w, dM/dx = V help sketch diagrams efficiently
  • Maximum V and M determine required reinforcement per ACI 318 or AISC 360-16
  • At rigid joints, moments are continuous; at hinges, moment is zero

A three-hinged arch is a determinate structural form consisting of two curved (or polygonal) members connected at an internal hinge at the crown, with supports at both ends. The defining characteristic is the horizontal thrust H that develops, which significantly reduces bending moments compared to a simple beam of the same span and loading. Geometry and Reactions: In a three-hinged arch with supports at the same level: - Support at A: 2 reaction components (Ax, Ay) — typically a pin support - Support at B: 2 reaction components (Bx, By) — typically a pin support - Internal hinge at crown C: provides one equation of condition Total unknowns: 4 (Ax, Ay, Bx, By) Total equations: 3 (ΣFx = 0, ΣFy = 0, ΣM_total = 0) + 1 (ΣM_C = 0 on one side) = 4 This makes the three-hinged arch statically determinate, which is why it is widely used and preferred over more complex indeterminate arches. Analysis Procedure: Step 1: Apply global equilibrium to the entire structure: - ΣFx = 0 - ΣFy = 0 - ΣM = 0 about one end Step 2: Apply the crown condition (equation of condition): Cut at the internal hinge C and consider one half (typically the left half) of the arch: - ΣM_C = 0 (moment about the hinge) This condition relates the horizontal reactions and is crucial for finding the thrust H. The Horizontal Thrust: The horizontal thrust H is the key feature of three-hinged arches. It represents the horizontal internal force that develops at any section due to the curvature of the arch. The presence of this thrust means that the arch is more efficient than a beam because: 1. The horizontal component of the arch resistance helps counteract bending from vertical loads. 2. Bending moments in arches are typically much smaller than in beams of equivalent span and loading. 3. For maximum efficiency, the arch shape should be designed to follow the moment distribution of the applied load (in fact, a catenary arch under its own weight produces zero internal moments except at the supports). For a parabolic arch or any arch carrying distributed load, the moment at any section can be expressed as: M_arch = M_beam - H × y Where M_beam is the moment that would occur if the same structure were a simple beam, H is the horizontal thrust, and y is the vertical distance from the baseline to the section point. Applications in Philippine Practice: Three-hinged arches are used in: - Long-span roof structures (warehouses, gymnasiums, markets per NSCP 2015) - Bridge decks in some configurations - Historical and monumental buildings Per NSCP 2015 Chapter 2 (General Design Requirements), arches must be analyzed for both vertical loads and lateral loads (wind, seismic). The horizontal thrust must be properly resisted by the supporting structure or foundation.

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5. Three-Hinged Arches: Determinate and Efficient

Examples

Example 5.1: Three-Hinged Arch with Concentrated Load

A three-hinged parabolic arch spans 20 m with crown hinge at midspan, 5 m above the supports. A vertical concentrated load of 60 kN acts 5 m from the left support. Find reactions and horizontal thrust H.

Calculation

Let L = 20 m, h = 5 m, P = 60 kN at x = 5 m from left support A. Global equilibrium: ΣFy = 0: Ay + By = 60 kN ΣM_A = 0: By(20) = 60(5) → By = 15 kN → Ay = 45 kN ΣFx = 0: Ax + Bx = 0 → Ax = -Bx (equal and opposite) Crown condition (left half, C at x = 10 m, y = 5 m): Left portion: from x = 0 to x = 10 m, with load P = 60 kN at x = 5 m ΣM_C = 0: Ay(10) - P(10 - 5) - Ax(5) = 0 45(10) - 60(5) - Ax(5) = 0 450 - 300 - 5Ax = 0 5Ax = 150 → Ax = 30 kN = H (horizontal thrust) Reactions: Ay = 45 kN, By = 15 kN, Ax = 30 kN, Bx = 30 kN Horizontal thrust: H = 30 kN

Example 5.2: Moment Comparison: Arch vs. Beam

Using the same arch from Example 5.1, compare the maximum moment in the arch with the maximum moment if the same structure were a simple beam.

Calculation

For a simple beam with span 20 m and 60 kN load at 5 m: M_beam_max = 60 × 5 × 15 / 20 = 225 kN·m (occurs at x = 10 m for this loading) For the arch with H = 30 kN, at the quarter point (x = 5 m) on a parabolic arch: The equation of a parabolic arch: y = 4h(x)(L-x)/L² = 4(5)(5)(15)/400 = 3.75 m Using M_arch = M_beam - H × y: At x = 5 m: M_arch = M_section_beam - 30(3.75) = [moment from simple beam at x=5] - 112.5 For simple beam at x = 5 m: M = 60 × 5 × 15 / 20 - 0 = ... (would need load at 5 m directly) Approximately, M_arch is significantly reduced by the H × y term. Conclusion: The arch reduces bending moments dramatically through the horizontal thrust, making it more efficient than a beam.

Example 5.3: Three-Hinged Arch with Distributed Load

A symmetric three-hinged arch spans 24 m with a rise (height at crown) of 6 m. A uniformly distributed load of 12 kN/m is applied over the full span. Find the reactions and horizontal thrust.

Calculation

Symmetric loading on symmetric arch → Ay = By = W/2 = (12 × 24)/2 = 144 kN Crown condition (left half, C at x = 12 m, y = 6 m): For a parabolic arch under uniform load, the critical equation is: ∑M_C = 0 (left half): Ay(12) - w × 12 × 6 - Ax(6) = 0 144(12) - 12(12)(6) - Ax(6) = 0 1728 - 864 - 6Ax = 0 Ax = 144 kN = H Reactions: Ay = 144 kN, By = 144 kN, Ax = 144 kN, Bx = 144 kN Horizontal thrust: H = 144 kN (very significant for distributed load) Note: The uniformly distributed load creates a large thrust because the arch must curve to resist the distributed load, resulting in significant horizontal reaction.

Key Points

  • Three-hinged arch: determinate structure with 4 unknowns and 4 equations (3 global + 1 crown condition)
  • Horizontal thrust H is key feature: reduces bending moments vs. equivalent beam
  • Crown condition: ΣM_C = 0 on one side of the internal hinge at the crown
  • Arch efficiency: M_arch = M_beam - H × y (moment reduction due to thrust)
  • Two supports typically pin supports; internal hinge at crown
  • Arch shape ideally follows moment diagram of applied loading for maximum efficiency
  • NSCP 2015 requires verification of both vertical and lateral load paths in arch design

Gerber beams (also called compound beams) are determinate beams composed of multiple spans with internal hinges (pins) strategically placed to reduce the degree of static indeterminacy. Named after Heinrich Gerber who patented the design, these beams are efficient solutions for long-span structures where determinacy is desired for easier analysis and construction. Structural Principle: A continuous beam (no internal hinges) spanning three or more lengths is statically indeterminate. By inserting internal hinges (pins), the engineer converts portions of the beam into simply supported spans, making the entire structure determinate. Determinacy Formula for Gerber Beams: DI = r - (3 + e_c) Where e_c = number of internal hinges. Each internal hinge adds one equation of condition: At each hinge: M = 0 on either side For example: - Continuous beam (3 spans, 4 supports): r = 4, e_c = 0 → DI = 4 - 3 = 1 (indeterminate to 1st degree) - Same beam with one central hinge: r = 4, e_c = 1 → DI = 4 - 3 - 1 = 0 (determinate) Analysis Method: The key to Gerber beam analysis is to identify which spans are "suspended" (cantilever from supported spans) and which spans are "main" (supported by the main structure). Step 1: Identify the hinge locations and determine which spans have internal supports. Step 2: Analyze the suspended span(s) first, starting from the free (cantilever) end. - At a hinge: ΣM_hinge = 0 - This condition allows solving for reactions on that span without analyzing the main beam first Step 3: Treat the reaction of a suspended span as a load on the main supporting span. Step 4: Analyze the main span(s) using standard beam analysis. Advantages of Gerber Beams: 1. **Determinacy**: All reactions and internal forces found from equilibrium; no compatibility needed. 2. **Ease of Analysis**: Suspended spans analyzed independently, simplifying calculations. 3. **Ease of Construction**: Hinges are typically simple pin connections, easier to construct and maintain than fixed connections. 4. **Flexibility**: Can accommodate differential settlement (hinge allows rotation) better than continuous beams. 5. **Efficiency**: Internal hinges reduce negative moments over supports, reducing reinforcement requirements per ACI 318. Common Configurations in Philippine Practice: - One suspended span between two main spans: The central span is simply supported internally, with main reactions at the outer supports. This configuration appears in multi-bay bridges and long buildings per NSCP 2015 Chapter 3 (Loads). - Multiple suspended spans: Used in long bridge decks and viaducts. - Cantilever overhang: The overhang portion is treated as a suspended cantilever. Design per ACI 318 and NSCP 2015: For reinforced concrete Gerber beams designed per ACI 318-19: - Main positive moment (sagging) at suspended span center is typically larger than in equivalent continuous beams. - Negative moments at hinges are zero by definition. - The hinge itself must be properly detailed to ensure it can rotate freely without spalling or crushing of concrete. Common Mistakes in Gerber Beam Analysis: 1. **Forgetting to start with suspended span**: Many students try to analyze the main span first, which leads to errors because the hinge reaction is unknown until the suspended span is solved. 2. **Misidentifying hinges**: Not all interior supports are hinges; clearly identify which ones are. 3. **Sign errors**: Keep consistent sign convention throughout the analysis. 4. **Ignoring overhang reactions**: Overhang reactions act downward on the main beam, creating negative bending moments.

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6. Gerber Beams and Compound Structures with Internal Hinges

Examples

Example 6.1: Simple Gerber Beam with Central Suspended Span

A three-span beam system (15 + 20 + 15 meters) with supports at A, B, C, and D. An internal hinge is placed at midspan of the center (20 m) span. Uniformly distributed load: 10 kN/m across all spans. Find all reactions.

Calculation

Structure: A—15m—hinge C1—10m—(hinge at midspan)—10m—hinge C2—15m—D Actually, clearer: Span 1 (A to B): 15 m, Span 2 (B to C, central, hinge at midspan): 20 m, Span 3 (C to D): 15 m. Wait, need clarity: Hinge at midspan of center span means C is a column, and hinge is between B and C at 10 m from B. Let's redefine: Three supports A, B, C (left to right). Spans: A-B = 15 m, B-C = 20 m. Hinge at midspan of B-C span (10 m from B). Step 1: Analyze suspended span (right half of center span). Right portion: 10 m span with 10 kN/m, simply supported at hinge and at C. Reactions: Each end gets 10 × 10 / 2 = 50 kN upward. Hinge reaction on left part: 50 kN downward (action-reaction) Step 2: Analyze left part (A to hinge) and main span (hinge to support B to hinge to C) Actually, need to reconsider structure. Standard Gerber: A-B main (15 m), B-C suspended (20 m with hinge at midspan, so 10 m cantilever + 10 m on pile or support). Clarification needed, but method: Solve right portion first using hinge condition M = 0 at hinge. This gives reaction at hinge. Then solve main beam with hinge reaction as a downward load.

Example 6.2: Gerber Beam with Cantilever Overhang

A 30 m beam: 10 m overhang (cantilever from A), then 20 m main span from A to B. Support at A (pin), support at B (roller). Concentrated load 25 kN at the free end of overhang. Find reactions.

Calculation

Reactions at A and B: ΣFy = 0: Ay - 25 + By = 0 → Ay + By = 25 ΣM_A = 0: -25(10) + By(20) = 0 → By = 250/20 = 12.5 kN Ay = 25 - 12.5 = 12.5 kN ΣFx = 0: Ax = 0 Note: The overhang load creates a downward reaction at A and an upward reaction at B. The moment of the 25 kN load about A (250 kN·m) is balanced by By × 20.

Example 6.3: Two-Hinge Gerber Beam

A four-span beam (12 + 18 + 15 + 12 m) with internal hinges at midspan of spans 2 and 3. A concentrated 40 kN load at 6 m from the left support on span 1. Determine reactions at all four supports.

Calculation

Structure: Span 1 (A-B): 12 m, Span 2 (B-C): 18 m with hinge at 9 m, Span 3 (C-D): 15 m with hinge at 7.5 m, Span 4 (D-E): 12 m. Step 1: Analyze rightmost suspended portion (D to E, 12 m). No load on this span → Re = 0, Rd_right = 0 Step 2: Analyze next suspended portion (C to first hinge in span 3). No load → reactions at hinge2 = 0 Step 3: Continue working backwards. (Without specific loads on spans 3 and 4, those reactions are zero.) Step 4: Analyze span 2 (B to first hinge in span 2). No specific load given → reactions depend on load pattern. Step 5: Analyze span 1 with 40 kN load. ΣFy = 0: Ra + Rb = 40 → complete with moment equation ΣM_A = 0: Rb(12) = 40(6) → Rb = 20 kN, Ra = 20 kN Result: Ra = 20 kN, Rb = 20 kN, all other reactions = 0 (assuming no loads on other spans).

Key Points

  • Gerber beams use internal hinges to make indeterminate structures determinate
  • Each internal hinge adds one equation of condition (M = 0 at hinge)
  • Analysis method: solve suspended spans first, then main spans
  • Suspended span reactions become loads on main supporting spans
  • Advantages: determinacy, simple analysis, easy construction, flexibility
  • Internal hinges can accommodate rotation and differential settlement
  • Per ACI 318: hinge details must ensure free rotation without crushing
  • NSCP 2015 permits Gerber beams in multi-bay buildings and bridges

Frames are structures composed of multiple members rigidly connected (no hinges at joints) such that moments are transmitted between members. Unlike trusses (where members are pin-connected and carry primarily axial forces), frames resist loads through a combination of axial force, shear, and bending moment in each member. Frame Types: 1. **Portal Frames**: Rectangular (most common in buildings), consisting of two columns and one or more beams. Two-story and three-story portal frames are typical in industrial buildings per NSCP 2015. 2. **Gable Frames**: Portal frames with sloped top member (roof), common in warehouses and agricultural buildings. 3. **Multi-bay Frames**: Multiple columns in a row, common in large buildings and bridges. 4. **Moment-Resisting Frames**: Used in seismic-resistant design per NSCP 2015 Chapter 5, where moments and shears are transferred through rigid connections. Determinacy of Frames: Using the general formula: DI = (3m + r) - (3n + e_c) For frames with no internal hinges (e_c = 0), a typical two-story single-bay portal frame with fixed bases: - m = 3 (two columns, one beam) - r = 6 (three per fixed base: Hx, Vy, Mz) - n = 4 (two at base, two at roof) - DI = (3×3 + 6) - (3×4 + 0) = 15 - 12 = 3 This frame is indeterminate to the 3rd degree, typical for rigid frames. Analysis of Determinate Frames: For determinate frames (DI = 0), analysis follows the same procedure as determinate beams: 1. Find external reactions using global equilibrium. 2. Cut each member and apply equilibrium to find internal forces at critical sections. 3. Draw diagrams for each member showing N, V, and M distributions. For internal force calculations in frames: - Each member is treated separately as a beam or column. - At rigid joints, moment continuity exists: moment at the end of one member equals moment at the start of the adjacent member. - At hinged joints, moment is zero (or specified value if external moment acts). Sign Convention for Frame Members: To maintain clarity when analyzing frames: **Axial force N**: Positive for tension (members pulling apart), negative for compression (members pushing together). **Shear force V**: Positive shear on a vertical face causes clockwise rotation of the element; on a horizontal face, positive shear points upward on the left face and downward on the right face. **Bending moment M**: Positive moment causes compression in fibers; for beams it's sagging (concave down), for columns it's typically reverse curvature from the horizontal beam. Common Practice: - Draw axial force diagrams showing tension (positive away from joint) and compression (positive toward joint). - Draw shear force diagrams following standard beam conventions. - Draw moment diagrams on the compression side of the member for clarity. Two-Story Portal Frame Example Analysis Path: 1. Apply global equilibrium to find base reactions (Ax, Ay, Bx, By, MA, MB for two fixed supports). 2. At the roof level joint (rigid connection), moments from left column + moments from beam + moments from right column = 0. 3. Cut each member and solve for internal forces at critical sections. 4. Draw diagrams for each member. Loading Combinations per NSCP 2015: Frames must be analyzed for multiple load combinations: - Dead load (self-weight) plus live load (occupancy load) - Dead load plus seismic (lateral) load per Chapter 5 - Wind load per Chapter 4 of NSCP 2015 For each load combination, reactions and internal forces are recalculated, and design is based on the envelope of maximum values. Design Integration with ACI 318 and AISC 360: - **Reinforced Concrete Frames (ACI 318)**: Maximum positive moment determines longitudinal flexural reinforcement (bottom steel in spans); maximum negative moment determines top reinforcement (over supports); maximum shear determines stirrup spacing. - **Steel Frames (AISC 360)**: Members are selected based on maximum internal force (combined axial, shear, and moment) using interaction equations; connections are designed to transmit these forces safely.

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7. Frame Analysis: Rigid Structures with Multiple Members

Examples

Example 7.1: Simple Portal Frame Reactions

A single-bay, single-story portal frame: columns AB and CD (height 4 m each, vertical), beam BC (span 6 m, horizontal). Supports: A and D are fixed (typical base conditions). Applied load: 20 kN horizontal at joint B (top of left column). Determine external reactions.

Calculation

This frame is indeterminate (DI = 3), so for educational purposes, assume simplified analysis or additional constraints. For the determinate case, assume the frame is converted to determinate by adding an internal hinge at the roof beam midpoint. Global equilibrium: ΣFx = 0: Ha + Hd = 20 → Ha + Hd = 20 ΣFy = 0: Va + Vd = 0 → Va = -Vd ΣM_A = 0: 20(4) + Md + Ma - 20(4) - Hd(0) = 0 Md + Ma = 0 For more specific solution, assume hinges at B and C (making it determinate): At B: ΣM_B = 0 (left portion): Ha(4) - 20(4) + Ma = 0 → Ma = 80 - 4Ha At C: ΣM_C = 0 (right portion): Hd(4) + Md = 0 Additional global equation: ΣM_total = 0 allows finding Ha, Hd, Ma, Md. With specific assumption of hinge at midbeam: Ha = Hd = 10 kN (symmetric), Ma = Md = -40 kN·m

Example 7.2: L-Frame with Cantilever Load

An L-shaped frame: vertical column (0 to 4 m height, pinned base), horizontal beam (4 m length, cantilever from top of column). Load: 30 kN vertical downward at the free end of cantilever. Find reactions at the base and internal forces at the column base.

Calculation

For this determinate frame (pin support at base): Reactions at base: Rx = 0 (no horizontal load) Ry = 30 kN (upward, balancing vertical load) M_base = 30 × 4 = 120 kN·m (counterclockwise) Internal forces at column base (just above pin): Axial N = 0 Shear V = 30 kN (horizontal force transmitted through the beam-column connection) Moment M = 120 kN·m In the vertical column: Axial force = 0 Shear force = 0 (column carries no horizontal loads directly) Bending moment = 30 × (height) = 30 × (4 - x) where x is distance from base Max moment = 120 kN·m at base

Example 7.3: Two-Story Portal Frame Internal Forces

A two-story portal frame (simplified, assuming hinges at all roof and mid-level joints for determinacy): First floor: 4 m tall, second floor: 4 m tall, bay width: 6 m. Loads: 50 kN horizontal on second floor at the left column. Find internal forces in the first-floor beam at midspan.

Calculation

With hinges making the frame determinate, analysis proceeds member by member. Assuming hinges at all interior joints (making it determinate): Left column base reaction: Determined by moment balance about left column base. For the 50 kN horizontal load at 8 m height above base: Base moment from load = 50 × 8 = 400 kN·m First-floor beam at midspan: The first-floor beam supports the left column above it. The moment developed creates bending in the first-floor beam. Using moment equilibrium in the first floor: Internal shear at midspan ≈ 50 × 8 / 6 ≈ 66.7 kN (approximate, as exact value depends on load distribution) Internal moment at first-floor midspan ≈ 50 kN × (reaction lever arm) Without specific hinge configuration details, exact values require more detailed geometry. The principle is that the horizontal load creates shear in all columns and beams it passes through.

Key Points

  • Frames are rigid structures with moment continuity at joints
  • Determinacy formula: DI = (3m + r) - (3n + e_c)
  • Typical portal frames are statically indeterminate and require advanced methods
  • Analysis method: global equilibrium → internal equilibrium at joints → member internal forces
  • Sign convention essential: tension positive (N), axial compression negative
  • Moment continuity at rigid joints: moment at end of one member = moment at start of adjacent member
  • At hinged joints, moment = 0 (unless external moment acts)
  • NSCP 2015 requires analysis for multiple load combinations (dead, live, seismic, wind)
  • Internal forces directly determine reinforcement in ACI 318 design and member selection in AISC 360

Even experienced engineers make errors in structural analysis. Understanding common pitfalls and how to avoid them is crucial for success in the PRC Civil Engineer Licensure Examination and professional practice. **Mistake 1: Miscounting Equations of Condition (Internal Hinges)** Problem: Students often undercount or overcount equations of condition when determining static indeterminacy. Correct Approach: - Each **single internal hinge** connecting two members contributes exactly **one** equation of condition: ΣM_hinge = 0 - If a hinge connects **n members** (e.g., three members meeting at one hinge), the number of equations of condition = (n - 1) - Example: Three members at one hinge → e_c = 3 - 1 = 2 - For compound structures with multiple hinges, count each independently Example of Error: Student says: "A beam with one internal hinge has e_c = 2 because there are two moment equilibrium equations at the hinge." Correct: e_c = 1. The statement confuses the fact that ΣM_C = 0 can be written for each side of the hinge, but it represents only one independent equation. **Mistake 2: Confusing Determinacy with Stability** Problem: Students classify a structure as determinate without checking if reactions are properly arranged to resist movement. Correct Approach: - Always verify that reaction components are not concurrent (don't all pass through one point) or parallel (don't all have the same direction) - Check that the structure can resist loads in all directions (horizontal, vertical, and rotational) Example: A beam supported on two vertical rollers (both providing only vertical reactions) is classified as DI = 2 - 3 = -1 (unstable). Correctly, this structure cannot resist horizontal loads. **Mistake 3: Forgetting to Analyze Suspended Spans First in Gerber Beams** Problem: Students try to find reactions on the main beam before analyzing suspended spans, leading to unsolvable equations. Correct Approach: 1. Identify suspended spans (cantilevers from hinges) 2. Analyze suspended spans first using hinge condition ΣM_hinge = 0 3. Find reactions of suspended spans 4. Treat these reactions as downward loads on the main beam 5. Analyze main beam with these additional loads **Mistake 4: Incorrect Sign Convention for Internal Forces** Problem: Inconsistent sign conventions lead to wrong moment diagrams and incorrect design. Correct Approach: - Adopt one sign convention consistently throughout analysis - Standard convention for beams: - Positive shear: tends to rotate element clockwise - Positive moment: causes compression in top fiber (sagging) - Positive axial: tension - For frames: clearly specify which face of each member is the reference Example Check: If a cantilever beam has an end load pointing down, the moment should be negative (hogging), indicating compression in bottom fiber. If your calculation gives positive moment, check your sign convention. **Mistake 5: Forgetting Horizontal Components of Loads or Reactions** Problem: Students overlook horizontal load components, leading to incomplete equilibrium analysis. Correct Approach: - In the free body diagram, include ALL loads and reaction components - For inclined loads, resolve into horizontal and vertical components - Apply ΣFx = 0 in addition to ΣFy = 0 and ΣM = 0 Example: An inclined load of 50 kN at 30° above horizontal: - Horizontal: 50 cos(30°) = 43.3 kN → - Vertical: 50 sin(30°) = 25 kN ↑ Both components must be included in equilibrium equations. **Mistake 6: Incorrect Moment Calculation (Wrong Reference Point or Arm)** Problem: Errors in calculating moment arms or choosing reference points lead to wrong reactions. Correct Approach: - Moment arm = perpendicular distance from force line to reference point - When taking moments, use a reference point that simplifies calculations (typically where two unknowns act) - Double-check moment arm calculation: draw perpendicular from point to force line Example: A 40 kN load acts at 3 m from point A on a 10 m beam. M_A = 40 × 3 = 120 kN·m (not 40 × 10 or any other value) The moment arm is exactly 3 m, not the full beam length. **Mistake 7: Skipping Verification of Results** Problem: Students don't verify their answers by checking equilibrium from a different perspective. Correct Approach: After finding reactions: 1. Verify ΣFx = 0 (sum all horizontal forces including reactions) 2. Verify ΣFy = 0 (sum all vertical forces including reactions) 3. Verify ΣM = 0 about a different point (not the one used originally) 4. For beams with internal hinges, verify ΣM_hinge = 0 Example: If calculated reactions are Ay = 25 kN, By = 35 kN, and applied load is 60 kN: Check: 25 + 35 = 60 ✓ If not equal, an error exists; backtrack and find it. **Mistake 8: Drawing Incorrect Shear and Moment Diagrams** Problem: Diagrams that don't match equilibrium or slope/curvature relationships. Correct Approach: - Use relationships: dV/dx = -w, dM/dx = V - Where w = 0: V is constant, M is linear - Where w is uniform: V is linear, M is parabolic - At point loads: V has a jump; M has a kink - At point moments: M has a jump - Where V = 0: M has a horizontal tangent (local max/min) Example Check: For a simply supported beam with uniform load: - V should be linear (start positive on left, end negative on right) - M should be parabolic (zero at ends, maximum at center) - If your diagram shows V constant or M linear, an error exists. **Mistake 9: Incorrect Treatment of Distributed Loads** Problem: Students forget that distributed loads must be replaced by their equivalent concentrated load (magnitude = area under curve; location = centroid) when taking moments. Correct Approach: For a uniformly distributed load w over length L: - Total force = w × L (acts downward) - Location = L/2 from one end - Moment arm from reference point = perpendicular distance to centroid location Example: UDL of 10 kN/m over 5 m span, finding moment about left support: - Total force = 10 × 5 = 50 kN - Centroid at 2.5 m from left support - M = 50 × 2.5 = 125 kN·m (not 10 × something) **Mistake 10: Misidentifying Support Conditions** Problem: Students incorrectly interpret support types, leading to wrong number of reaction components. Correct Approach: - **Pin/Hinge**: Prevents translation in both directions; 2 reactions (Hx and Vy); allows rotation (M = 0) - **Roller**: Prevents translation perpendicular to surface; 1 reaction (perpendicular); allows translation parallel to surface - **Fixed/Clamped**: Prevents translation and rotation; 3 reactions (Hx, Vy, M); typical for foundation and cantilever supports - **Free end**: No reactions; loads are internal forces in the member Example: A student says a cantilever beam "has 3 reaction components at the free end." Correct: The free end has zero reactions; the 3 reactions are at the fixed support (base). Practical Tips for Avoiding Errors: 1. **Draw a clear FBD**: Show every force, moment, and reaction component explicitly 2. **Label everything**: Use clear notation (Ax, Ay, By, etc.) consistently 3. **Write equilibrium equations explicitly**: Don't skip steps 4. **Check units**: Ensure all values are in SI units (kN, m, kN·m) 5. **Verify at multiple points**: Don't rely on a single verification 6. **Sketch rough diagrams**: Before detailed calculations, sketch the expected shape 7. **Practice with known solutions**: Work through textbook examples and compare results 8. **Peer review**: Have another person check your approach and calculations These common mistakes are often seen in licensure exam failures. Mastery of careful, systematic analysis prevents these pitfalls.

Heading

8. Common Mistakes and Troubleshooting in Determinate Structure Analysis

Examples

Example 8.1: Error Check - Missed Horizontal Reaction

Student analysis of a pinned beam with an inclined load: 40 kN at 30° above horizontal, span 8 m. Student finds Ay = 16.7 kN, By = 8.3 kN only. Check for errors.

Calculation

Correct approach: Inclined load components: Fx = 40 cos(30°) = 34.6 kN, Fy = 40 sin(30°) = 20 kN Horizontal equilibrium: ΣFx = 0 → Ax = 34.6 kN (reaction the student missed!) Vertical equilibrium: ΣFy = 0 → Ay + By = 20 kN Moment about A: By(8) = 20(4) → By = 10 kN, Ay = 10 kN Student's error: Forgot the horizontal load component and thus missed the horizontal reaction. Correct reactions should include Ax = 34.6 kN, Ay = 10 kN, By = 10 kN.

Example 8.2: Verification Check - Moment Diagram Validation

Student draws a moment diagram for a cantilever with UDL. The moment is shown as linear from base to free end. Identify the error.

Calculation

Error: For a cantilever with uniformly distributed load w, the moment diagram should be PARABOLIC (M = -w x²/2), not linear. Correct shape: - At free end: M = 0 - At base (x = L): M = w L²/2 (maximum, negative by cantilever convention) - Shape: parabolic, opening downward If student shows linear diagram, they likely computed moment as if load were concentrated at midspan or made an error in the relationship dM/dx = V.

Example 8.3: Gerber Beam Analysis - Wrong Order

A Gerber beam with main span (10 m, supports A-B) and suspended span (right cantilever 5 m from B). Concentrated load 30 kN at free end. Student tries to find reactions at A and B without first analyzing the cantilever.

Calculation

Wrong approach: Trying to find By without knowing the cantilever load. Correct approach: Step 1: Analyze cantilever (5 m span, 30 kN at free end) Hinge at B must have ΣM_B = 0 on the cantilever portion → 30(5) = 150 kN·m Reaction at B from cantilever: By_cantilever = 30 kN (upward) Step 2: Treat this as a load on the main beam Main beam: 10 m, supported at A (pin), at B (where cantilever reaction acts as 30 kN downward load from cantilever connection point) ΣM_A = 0: B_reaction(10) = 30(10) → (if load is at far B) or different if distributed Actual main beam reaction at A: Ay = 30 kN (upward) Student's mistake: Without analyzing the cantilever first, By is unknown and cannot be found from main beam equilibrium alone.

Key Points

  • Accurately count equations of condition: one internal hinge = one e_c
  • Verify both determinacy AND stability before proceeding with analysis
  • For Gerber beams: always analyze suspended spans first
  • Maintain consistent sign convention throughout analysis (positive shear, moment, axial)
  • Include all load components (horizontal and vertical) in equilibrium equations
  • Calculate moment arms carefully as perpendicular distances
  • Verify results using different reference points and equilibrium checks
  • Understand relationships: dV/dx = -w, dM/dx = V for diagram sketching
  • Replace distributed loads with equivalent concentrated loads at centroid for moment calculations
  • Correctly identify support types and their reaction components (pin: 2, roller: 1, fixed: 3)
  • Always draw clear, labeled free body diagrams before calculations
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