Module 01 of 06

35 minutes

Beam types, load paths and idealization

Compare five beam systems, select defensible supports, trace load paths and state the boundary of the model.

Suggested pacing · 35 minutes
  1. Illustrated systems and worked workshop15 min
  2. Comparison and calculation record15 min
  3. Knowledge check5 min

Work at your pace and record actual engaged time. Optional references and extensions may take longer.

A beam solver answers the mathematical problem it is given. The engineer’s first task is therefore not pressing Run; it is deciding which physical behaviours belong in the idealized model.

Start with the load path

Trace each load from its point of application to the supports. Record what transfers shear, what transfers axial force, and whether the connection can develop a meaningful couple. A clean sketch with dimensions and restraint directions is more valuable than an early, polished response diagram.

The modeling sequence
  1. Define the member centreline and analysis extent.
  2. Identify the restraints the surrounding structure can actually provide.
  3. Apply loads at their physical locations and over their real tributary lengths.
  4. Assign material and section stiffness consistently.
  5. State what the model omits before interpreting the result.

Recognize the beam system before choosing a formula

A beam type is defined by its support and continuity conditions—not by whether the member is steel, timber or concrete. The same cross-section can behave as a simple span, cantilever or continuous member depending on how it connects to the surrounding structure. That distinction controls the reaction set, bending-moment pattern and appropriate verification equations.

Guide-to-course field atlas

Five beam systems, from real structure to benchmark

Use the same sequence for every system: recognize the physical load path, assign restraints, predict the response, check a reference case, then challenge the assumption most likely to invalidate the model.

Simply supported

Determinate
Simply supported beam on a pin and roller under distributed load with shear, moment and deflection diagrams

Where it appearsBridge girders on bearings, joists bearing on walls, lintels and beams with simple shear connections.

Ideal modelPin at A and roller at B. Vertical displacement is restrained at both ends; rotation remains free; one end can accommodate longitudinal movement.

Response signatureZero ideal end moments. A symmetric downward UDL produces equal reactions, positive sagging moment and a symmetric downward elastic curve.

Full-span UDL on span L

RA = RB = wL/2
Mmax = wL2/8
δmax = 5wL4/(384EI)

Assumption to defendDo not assume “simple” merely because a connection is drawn with bolts. Confirm that connection and surrounding-frame rotational stiffness are negligible for the result being checked.

Open the complete simply supported guide

Cantilever

Determinate
Cantilever beam fixed at one end with load and shear, moment and deflection diagrams

Where it appearsBalconies, entrance canopies, mast arms, brackets, retaining-wall stems and projecting roof elements.

Ideal modelOne end restrains translation and rotation; the other is free. The support must deliver shear, axial force when present and a moment couple.

Response signatureFor downward transverse loading, moment magnitude grows toward the fixity and the largest displacement normally occurs at the free tip.

Point load P at the free tip

VA = P
MA = −PL
δtip = PL3/(3EI)

Assumption to defendThe wall, column, base plate or foundation may rotate. A perfectly fixed symbol can seriously understate deflection when the supporting system is flexible.

Open the complete cantilever guide

Fixed–fixed

Indeterminate
Fixed beam restrained at both ends under distributed load with shear, moment and deflection diagrams

Where it appearsMonolithic concrete frames, moment-frame girders and machine members clamped by sufficiently stiff supports.

Ideal modelVertical displacement and rotation are restrained at both ends. Compatibility and EI are required to determine the end moments.

Response signatureGravity load creates hogging at the supports, sagging in the span and substantially less deflection than the equivalent simple span.

Full-span UDL on span L

RA = RB = wL/2
MA = MB = −wL2/12
Mmid = +wL2/24
δmid = wL4/(384EI)

Assumption to defendFixity is a stiffness assumption—not a connection label. Check the joint, columns or walls, foundations and adjacent framing that must supply rotational restraint.

Open the complete fixed–fixed guide

Overhanging

Usually determinate
Overhanging beam extending past an inboard support with response diagrams

Where it appearsRoof eaves, platform edges, canopy beams and framing that projects beyond the last column or bearing.

Ideal modelA pin and roller lie inside the member length, leaving a free projection. The support span is L and the overhang length is a.

Response signatureOverhang loading creates negative moment at the inboard support and can reverse the remote reaction, demanding a real uplift load path.

Point load P at the overhang tip

RA = −Pa/L
RB = P(L+a)/L
MB = −Pa
δtip = Pa2(L+a)/(3EI)

Assumption to defendA negative reaction is not only a sign convention. Bearing-only contact cannot pull on the beam; add a hold-down, stabilizing load or a different support model.

Open the complete overhanging guide

Continuous

Indeterminate
Two-span continuous beam passing over three supports with response diagrams

Where it appearsMulti-span bridge girders, floor beams over columns and roof purlins passing across several frames.

Ideal modelOne uncut member passes over three or more supports. Adjacent spans share rotation at an interior support, so their responses are coupled.

Response signatureContinuity creates negative interior-support moment, redistributes reactions and usually reduces balanced-load positive moment and deflection.

UDL w on two equal spans ℓ

RA = RC = 3wℓ/8; RB = 5wℓ/4
MB = −wℓ2/8
M+max = 9wℓ2/128

Assumption to defendMembers touching at a support are not automatically continuous. Moment must pass through an uncut section or a connection capable of sustaining the required rotation compatibility.

Open the complete continuous guide

How to use the references: the equations are benchmark cases, not universal beam formulas. They are valid only for the stated geometry, loading, constant EI and boundary conditions. The dedicated guides add live diagrams, alternate load cases and full worked calculations; this course asks you to compare, predict and document the five systems in one review workflow.

Quick reference: compare the five systems
Beam systemIdealized boundaryDeterminacy and characteristic responseTypical modeling trap
Simply supportedPin at one end, roller at the otherStatically determinate; idealized end moments are zeroAdding end fixity that the bearings or shear connections cannot provide
CantileverFixed at one end, free at the otherStatically determinate; maximum moment commonly occurs at the fixed endIgnoring rotation or flexibility of the supporting column, wall or base
OverhangingTwo supports with member extending past one or bothUsually determinate; overhang loading can reverse a reaction and create support-region hoggingAssuming a bearing can resist uplift after a reaction changes sign
Fixed–fixedRotation and translation restrained at both endsIndeterminate; end moments reduce positive span moment and deflectionTreating nominally rigid joints as perfectly fixed without stiffness evidence
ContinuousOne member over three or more supportsIndeterminate; continuity creates negative support moments and redistributes responseSplitting the member into independent simple spans and losing continuity
Determinacy in practical terms

If equilibrium supplies enough independent equations to recover the reactions, the system is statically determinate. If extra restraints introduce more unknown actions, deformation compatibility and stiffness are needed. Indeterminate does not mean “better” or “more advanced”; it means the response depends on both equilibrium and how the structure deforms.

A four-question beam-type screen

  1. Where can the member translate, and where can it rotate?
  2. Does the member continue through a support, terminate there, or project beyond it?
  3. Can the connection actually develop the modeled moment or uplift force?
  4. Would support settlement, joint flexibility or loss of contact change the load path?

Read the restraint before drawing the reaction

A support symbol is a compact statement about movement. In a two-dimensional frame model, a beam-end node can translate horizontally, translate vertically and rotate. Restraining any one of those degrees of freedom introduces the corresponding possible reaction component; whether that reaction is non-zero depends on the load case.

Degrees of freedom → reactions

Convert physical behavior into three model decisions

  1. 1
    Identify allowed movementCan the node move in x, move in y, or rotate?
  2. 2
    Mark each restraintA restraint imposes a displacement boundary condition.
  3. 3
    Draw possible reactionsRestrained translation creates force; restrained rotation creates moment.
Three possible movements at a two-dimensional beam nodeA beam-end node can translate horizontally, translate vertically and rotate. Restraining those movements creates horizontal reaction, vertical reaction and moment reaction respectively.ONE BEAM-END NODEuₓhorizontaluᵧverticalθrotationRESTRAINED MOVEMENT → POSSIBLE REACTIONrestrain uₓreaction Rₓrestrain uᵧreaction Rᵧrestrain θreaction M
Teal = allowed movementAmber = restrained movement and possible reaction

Three common idealizations

Symbol, physical realization and model consequence

Start with what the connection lets the beam do, then add only the reaction components associated with restrained movement.

01

Roller support

Carries force normal to its bearing surface while allowing movement along the bearing and end rotation.

Roller support application: bridge expansion bearingA bridge girder rests on a roller bearing over a concrete pier. The support carries vertical reaction while allowing thermal movement.BRIDGE EXPANSION BEARINGRᵧMOVEMENT ALLOWEDROTATION ALLOWED
Moves freely
Tangential translation ut and rotation θ
Restrains
Normal translation un = 0
Possible reactions
Rn · one force normal to the surface
Beam-end condition
Horizontal beam end: v = 0; M = 0 if no end couple is applied
Field test

Can the physical bearing slide in the modeled direction without binding?

Modeling cautionA roller reaction is normal to the bearing surface; it is not automatically vertical.

02

Pinned support

Holds the beam-end node in place while allowing it to rotate without an idealized moment reaction.

Pinned support application: simple beam-to-column connectionA beam is connected to a column through a simple shear plate and pin. Translation is restrained while end rotation remains possible.SIMPLE SHEAR CONNECTIONRᵧRₓROTATION ALLOWED
Moves freely
Rotation θ
Restrains
ux = 0 and uy = 0
Possible reactions
Rx, Ry · two force components
Beam-end condition
Beam end in bending: v = 0; M = 0 if no end couple is applied
Field test

Is connection moment small enough to neglect for the result being checked?

Modeling cautionA support pin restrains a node relative to ground. An internal hinge joins members and releases transferred moment; they are not interchangeable.

03

Fixed support

Prevents translation and rotation, so the connection must transfer force and a moment couple into the supporting system.

Fixed support application: cantilever cast into a wallA cantilever beam is embedded into a wall. Horizontal and vertical translation and end rotation are restrained.RIGID CANTILEVER CONNECTIONRᵧRₓM
Moves freely
No movement in the idealized 2D model
Restrains
ux = 0, uy = 0 and θ = 0
Possible reactions
Rx, Ry, M · two forces plus moment
Beam-end condition
Beam end: v = 0 and dv/dx = 0
Field test

Which connection, column, wall or foundation supplies the modeled moment restraint?

Modeling cautionReal connections are often semi-rigid. Perfect fixity is credible only when the complete supporting system is sufficiently stiff.

State the theory boundary

The calculator’s classical beam response assumes a small-displacement, linear-elastic idealization. The member centreline, support locations, applied loads, modulus of elasticity and section properties must be internally consistent. Local connection deformation, lateral-torsional behaviour, shear deformation, material yielding, construction sequence and load redistribution may require separate treatment.

Common failure mode

A shear connection is modeled as fixed because the software’s default support looked convenient. The model becomes artificially stiff, end moments appear, midspan moment falls, and deflection is suppressed. The output can be numerically precise while representing the wrong structure.

Worked comparison 01

Same 6 m beam. Three different answers.

Use w = 8 kN/m, E = 200 GPa and I = 200 × 106 mm4. Only the boundary conditions change. Compare physical patterns first; modules 2–4 develop the calculations.

Simply supported

Pin and roller; end rotation is free.

8 kN/m · full 6 m span↑ 24 kN↑ 24 kNDEFLECTIONShape exaggerated · 3.375 mm maximumBENDING MOMENT · kN·m0+36Positive above zero · each plot scaled independently
Reactions
RA = RB = 24 kN
Moment
Mmax = wL²/8 = 36 kN·m
Deflection
δmax = 3.375 mm

Fixed–fixed

End rotations are restrained.

8 kN/m · full 6 m span↑ 24 kN↑ 24 kNDEFLECTIONShape exaggerated · 0.675 mm maximumBENDING MOMENT · kN·m0+12−24−24Positive above zero · each plot scaled independently
Reactions
RA = RB = 24 kN
Moments
Mend = −24; Mmid = +12 kN·m
Deflection
δmid = 0.675 mm

Cantilever

One fixed end carries all actions.

8 kN/m · full 6 m span↑ 48 kNDEFLECTIONShape exaggerated · 32.4 mm maximumBENDING MOMENT · kN·m0−144free tipPositive above zero · each plot scaled independently
Fixed reaction
V = 48 kN
Moment
Mfixed = −wL²/2 = −144 kN·m
Deflection
δtip = 32.4 mm

Engineering takeaway: equilibrium recovers the same 48 kN total load in all three cases, yet maximum absolute moment demand ranges from 24 kN·m (fixed–fixed) through 36 kN·m (simple span) to 144 kN·m (cantilever), and deflection from 0.675 to 32.4 mm. Selecting the wrong boundary condition can change the governing conclusion.

Five-model beam-type comparison lab

Use the comparison-and-record part of your activity plan for this lab. Before opening each model, sketch its supports, expected deflected shape and where positive or negative moment should occur. Prioritize the simple/fixed pair, then check the other systems. The goal is a mental library of response patterns, not memorizing isolated maximum values; record any additional study time.

Prepared systemPrediction to write firstOpen model
6 m simple span, 8 kN/m UDLEqual reactions; zero end moment; symmetric positive moment and downward deflectionSimply supported model →
3 m cantilever, 24 kN tip load24 kN base shear; 72 kN·m base moment; largest deflection at the free tipCantilever model →
6 m fixed–fixed beam, 8 kN/m UDLEqual reactions; negative end moments; smaller positive span moment and deflection than the simple spanFixed–fixed model →
Two-span continuous beam, 8 kN/m UDLNegative moment over the centre support and positive moment in both spansContinuous model →
6 m span + 2 m overhang with tip loadPossible uplift at A; large negative moment at B; largest movement near the free tipOverhanging model →
  1. Verify the supports, span dimensions and loading before looking at any result.
  2. For each system, mark the reaction directions and all locations where moment must be zero or where rotation is restrained.
  3. Compare the simple and fixed–fixed UDL cases. Both carry 48 kN total, but their moment and deflection patterns differ because their boundary conditions differ.
  4. Compare the continuous and overhanging cases at the inboard support. Explain why both can show negative moment while the physical mechanisms are different.
  5. Identify which two models cannot be solved completely by equilibrium alone and name the compatibility information the solver must enforce.
Reveal the comparison reference

The simple span and cantilever are determinate. The fixed–fixed and continuous models are indeterminate and require stiffness plus compatibility. The overhang is determinate but can demand uplift restraint. For the symmetric UDL cases, the simple-span maximum moment is wL²/8 = 36 kN·m. The fixed–fixed reference has end moments of magnitude wL²/12 = 24 kN·m and positive midspan moment of magnitude wL²/24 = 12 kN·m. The reduction is a consequence of rotational restraint, not a change in applied load.

Required workbook evidence

Create a five-row comparison table with beam type, determinacy, expected reaction pattern, moment boundary conditions, deflected-shape description and one physical assumption that could invalidate the model. This is the principal activity for the 35-minute module.

Practice: write the model statement

Choose a real beam from your work or studies and write one sentence for each item: analysis extent, supports, loads, stiffness, expected response and excluded behaviours. Challenge each support with the question “what surrounding component supplies this restraint?” This six-line record is the beginning of your calculation audit trail.

Open the illustrated beam-types reference

Workshop 1 · From a detail to an analysis decision

What must be true for your support symbol to be credible?

A project sketch labels a beam “supported by a steel column.” That description tells you where the force goes, but does not establish rotational restraint. A seat, shear tab, end plate and welded moment connection can all connect a beam to a column and produce different behaviour. Begin with the connection detail and the stiffness of everything behind it. A strong connection attached to a flexible column does not create an infinitely rigid boundary.

For this exercise, picture a 6 m floor beam carrying a uniformly distributed 8 kN/m service load. Its left bearing locates the member horizontally; the right bearing can slide. Both bearings allow rotation. The idealization is a pin and roller. Label A and B at the actual bearing centrelines, and identify which member length belongs in the calculation. A beam that physically extends beyond the bearings has an overhang even if the drafting label says “simple beam.”

Worked decision: a credible simple support

  1. State the observed detail. Both ends transmit vertical shear. No designed moment couple or significant rotational stiffness is established. One bearing accommodates axial movement.
  2. Translate it into conditions. At A: u = 0 and v = 0. At B: v = 0. Neither support imposes θ = 0. For this load case, axial reaction is zero, although the pin could carry horizontal force under another load.
  3. Predict before calculating. Under a symmetric UDL, both reactions are upward and equal, bending is sagging, end moment is zero, and downward deflection peaks at midspan.
  4. Calculate a benchmark. R = 8(6)/2 = 24 kN. Mmax = 8(6²)/8 = 36 kN·m. A fixed–fixed calculation produces the same vertical reactions, so equilibrium alone cannot choose between the models.
  5. Identify evidence that could change the decision. Obtain the actual connection and bearing details. If they establish meaningful restraint, compare a justified stiffness model with the simple-span benchmark and document the sensitivity.

Stability and determinacy are separate checks

For a planar rigid body, three independent equilibrium equations are available. A conventional pin plus horizontal roller supplies three appropriately arranged restraints. Replacing the pin with a second horizontal roller leaves horizontal rigid-body translation unrestrained. Adding restraints may make the system indeterminate, but counting reaction components alone is not a proof of stability: their directions and locations matter.

A model can also become unstable when a support loses contact. A roller symbol that permits a downward reaction implicitly represents a device capable of pulling on the member. A plain bearing cannot do that. The capstone will deliberately expose this difference. Treat stability as a property of the member, restraints and load case together.

Predict the consequences of continuity

Now imagine the same physical member continues across a middle support. An uncut section enforces displacement and rotation compatibility across that location. The support can have zero external moment reaction while the continuous beam has a non-zero internal bending moment there. “Roller support” does not mean “internal hinge.” Inserting a hinge releases moment transfer; splitting the beam into separate spans changes the structure being solved.

A model statement another engineer can use

“Analyze the 6 m centreline span as a prismatic Euler–Bernoulli beam with constant EI, small displacements and linear elastic response. Use a pin at A and a vertical roller at B, justified by rotating bearings with axial movement at B. Apply the stated 8 kN/m service load once. Exclude connection deformation, lateral stability and member resistance from this calculation.”

Your decision exercise

Use the three-boundary comparison above to calculate the required values in the activity record. Your explanation should say what detail would justify fixing the ends, what effect that would have on moments and displacement, and what would remain unchecked. Write the statement before inspecting the reference wording. This is the first entry in your saved calculation workbook.

Optional extension · A spring between pin and fixed

A real joint can be represented by a rotational spring with stiffness kθ. Comparing kθ with EI/L helps identify whether joint rotation is likely to matter; the ratio kθL/EI is dimensionless. A low ratio approaches a released rotation, and a high ratio approaches rotational restraint. Neither limit supplies a universal cutoff: choose a model whose sensitivity is acceptable for the actual decision. Investigate this only after completing the core comparison; extra study time is recorded separately from the planned activity budget.

Required calculation record · Module 1

Defend a support model

A 6 m floor beam carries 8 kN/m. Draw a pin at A and roller at B, then compare with an ideal fixed–fixed model. Use the full-span UDL benchmarks above.

Use a calculator and your notes. Enter numbers in the stated units, without unit text or thousands separators. Your calculations receive numerical feedback; your written reasoning is retained in the workbook and is not individually instructor-graded.

This is the exercise included in the free preview. Work it on paper; enrollment adds a study-time log, saved calculation records and a certificate after successful course completion.

Build your CPD / PDH study-time record as you go. Exclude breaks and idle time; record actual learning time against the three-hour course plan. Include your knowledge-check time; assessment time can be added on the final form.

Continue the course

Work toward your hours and completion certificate.

$99 USD, paid once. Follow the 3-hour CPD / PDH learning plan, record your actual study time and receive your personalized certificate after completing the activities and passing the assessment.

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