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Chapter 6 • Theory & Derivations

Influence Lines and Moving Loads

Comprehensive university textbook unit covering fundamental theory, mathematical derivations, numerical modeling, and design validation of Influence Lines and Moving Loads. Developed for undergraduate civil engineering study.

§6.1 Conceptual overview

Conceptual overview

An influence line plots a response quantity at a fixed location while a unit load moves through a structure. It is not the same as a bending-moment diagram under one fixed loading arrangement. Influence lines translate moving-load problems into evaluation of response ordinates at successive axle positions. For a statically determinate simply supported bridge, reaction influence lines are linear, and a section-moment influence line is triangular. For indeterminate bridges, continuous support compatibility influences the shape. Numerical stiffness analysis can move unit loads through the mesh to obtain ordinates. Care is needed when point loads fall inside finite elements; a consistent nodal load projection should preserve virtual work, not merely allocate the full force to the nearest node.

§6.2 Learning outcomes

Learning outcomes

After working through this unit you should be able to: (1) construct a physically consistent idealization, (2) express the relevant force, stiffness and displacement variables using compatible units, (3) solve a demonstrative problem by hand or a transparent numerical method, (4) interpret response patterns and their sensitivity to input parameters, and (5) identify what the simplified model cannot prove. In this unit the most important observation is not merely a numerical answer but the connection between structural behavior and the assumed support or constitutive conditions.

§6.3 Unit engineering case — Bridge truck crossing

Unit engineering case — Bridge truck crossing

A two-axle vehicle enters and exits a simply supported deck span. Compute end reactions and midspan bending moment at several axle positions, including a position with one axle off the span. Confirm the piecewise moment function and note the section of maximum curvature under the assumed simple-span linear model. Describe the additional factors required for traffic design: dynamic amplification, multiple vehicle lanes, load distribution between girders and prescribed load patterns.

Investigation sequence

Begin by preparing a diagram that names every member, support, load, imposed movement and unknown. Choose an independent coordinate system and assign a sign to every generalized force. Derive a minimal reference calculation before using a computational model. Then run a sensitivity study in which only one physical assumption changes at a time. Record both the predicted movement and the reaction or internal-force counterpart. Check conservation of force and moment where the physical model supports those checks. Finally compare the calculation with a plausible measurement or with a more complete independent model. Label the evidence as a verification benchmark, an assumption or a genuinely observed fact.

Suggested written report

A useful report has a one-paragraph engineering question, a table of parameter values with units, an explicit statement of boundary conditions, the governing equations, a readable figure of the system, a table of numerical results, at least one independent verification, and a conclusion that identifies unverified assumptions. State what happens when the governing input doubles, when stiffness increases, and when a support is relaxed or stiffened. Explain whether the observed changes follow from algebraic scaling or from a change in load path. Keep the original units in the file even if a graph displays a converted unit.

§6.4 Reaction influence lines

6.1 Reaction influence lines

Learning target and physical interpretation

For a single span with two simple supports, a unit moving vertical load produces end reactions proportional to distance from the opposite support. The response changes continuously along the span.

Governing relation

RA(x)=(L−x)/L and RB(x)=x/L for unit downward load at 0≤x≤L.

Worked engineering interpretation

On a 20 m span a unit load at x=7 m creates reactions RA=0.65 and RB=0.35 in consistent force units.

What the idealization omits

The ordinate is a reaction per unit moving load, not a real reaction until multiplied by the axle magnitude.

Verification and interpretation of results

Test endpoints: RA(0)=1, RA(L)=0, and RA+RB=1 at every intermediate position.

Applied case and decision boundary

Compare how a weighbridge axle position changes load sharing between two bearings. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: The ordinate is a reaction per unit moving load, not a real reaction until multiplied by the axle magnitude. Explain which physical check exposes the error.

5. Professional judgment: Using the case Compare how a weighbridge axle position changes load sharing between two bearings., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

§6.5 Section moment influence line

6.2 Section moment influence line

Learning target and physical interpretation

A fixed-section bending moment depends on where the moving load lies relative to that section. The resulting influence line is piecewise linear for a simple span.

Governing relation

For section a, ordinate y_M(x)=x(L−a)/L for x≤a and a(L−x)/L for x≥a.

Worked engineering interpretation

For L=20 m and a=8 m, the peak unit-load moment ordinate occurs at x=a and equals a(L−a)/L=4.8 m.

What the idealization omits

Confusing the plotted x-coordinate of the load with the section coordinate a may turn a triangular influence line into the wrong bending diagram.

Verification and interpretation of results

Check continuity at x=a and zero influence at x=0 and x=L, then multiply each axle load by its ordinate.

Applied case and decision boundary

Explain why the governing position for one concentrated axle is directly above the section. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: Confusing the plotted x-coordinate of the load with the section coordinate a may turn a triangular influence line into the wrong bending diagram. Explain which physical check exposes the error.

5. Professional judgment: Using the case Explain why the governing position for one concentrated axle is directly above the section., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

§6.6 Two-axle train on a bridge

6.3 Two-axle train on a bridge

Learning target and physical interpretation

A moving vehicle changes the load positions in a fixed coordinate system. Reactions are calculated from moment equilibrium using only axles currently on the structure.

Governing relation

RB=Σ(P_i x_i/L), RA=Σ P_i−RB, and M(s)=RA s−Σ_{x_i≤s}P_i(s−x_i).

Worked engineering interpretation

For a 20 m span carrying 80 kN at x=9 m and 110 kN at x=5 m, RB=(80×9+110×5)/20=63.5 kN and RA=126.5 kN.

What the idealization omits

Including an axle after it has left the bridge makes both reaction and moment equilibrium wrong; the load entry and exit cases must be explicit.

Verification and interpretation of results

Use Lab 10 to move the front axle across the bridge and check reaction sums when only one axle lies on the span.

Applied case and decision boundary

Investigate the difference between maximum midspan moment and maximum shear near a support. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: Including an axle after it has left the bridge makes both reaction and moment equilibrium wrong; the load entry and exit cases must be explicit. Explain which physical check exposes the error.

5. Professional judgment: Using the case Investigate the difference between maximum midspan moment and maximum shear near a support., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

§6.7 Envelopes and spacing effects

6.4 Envelopes and spacing effects

Learning target and physical interpretation

A response envelope is the extreme over all permitted positions and load configurations, not a diagram for one arbitrary vehicle position. Closely spaced axles may create higher local moments.

Governing relation

For a set of axle positions {x_i(a)}, M_max(s)=max_a M(s;a), subject to the placement constraints.

Worked engineering interpretation

An axle train with two heavy close-spaced loads may govern a near-midspan section even if the heaviest individual axle alone governs a different section.

What the idealization omits

Optimizing only the load position but not wheel spacing is insufficient when multiple vehicle configurations are possible.

Verification and interpretation of results

Compute an envelope on a grid of positions, then refine around peaks to avoid grid-discretization bias.

Applied case and decision boundary

Describe the role of lane distribution and dynamic allowance in a real bridge loading specification. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: Optimizing only the load position but not wheel spacing is insufficient when multiple vehicle configurations are possible. Explain which physical check exposes the error.

5. Professional judgment: Using the case Describe the role of lane distribution and dynamic allowance in a real bridge loading specification., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

§6.8 Continuous-span moving-load model

6.5 Continuous-span moving-load model

Learning target and physical interpretation

On a continuous beam a moving axle can influence negative support moments as well as positive span moments. Stiffness analysis or closed-form influence surfaces may be required.

Governing relation

For a loaded beam element, a point force at local coordinate ξ contributes f_e=P [N1(ξ),N2(ξ),N3(ξ),N4(ξ)] with cubic Hermite shape functions.

Worked engineering interpretation

Moving a load from the center of the left span to the center of the right span can reverse the relative contribution to the interior support moment of a two-span bridge.

What the idealization omits

Placing a point force on whichever mesh node happens to be nearest introduces an artificial force-position jump and distorts influence lines.

Verification and interpretation of results

Repeat with refined elements and test convergence of the support-moment response at the same physical axle locations.

Applied case and decision boundary

Outline how a highway bridge software verification model can use a simple-span influence line as a baseline. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: Placing a point force on whichever mesh node happens to be nearest introduces an artificial force-position jump and distorts influence lines. Explain which physical check exposes the error.

5. Professional judgment: Using the case Outline how a highway bridge software verification model can use a simple-span influence line as a baseline., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

§6.9 End-of-unit self-check

End-of-unit self-check

  1. Which unknown in the five lesson models is governed principally by equilibrium, and which requires a deformation condition? Explain for two different examples.
  2. Identify a boundary-condition assumption in this unit that could change if a real bearing loses contact or a joint begins to slip.
  3. Form a dimensionless or unit-consistent ratio from a model response and a characteristic load or span, then explain how that ratio changes with structural stiffness.
  4. Explain how a model could satisfy overall force balance and nevertheless predict the wrong deformation field.
  5. Design a two-point numerical verification plan that does not reuse the same solver for both checks.
  6. Identify the limitation of treating code design or material yielding as if it were included in these ideal elastic analyses.

Short answer guidance: A complete answer should use a named force path or deformation coordinate rather than generic phrases. A verification answer should specify the numerical quantity being compared and the expected reference; a validation answer should identify a relevant observation or tested physical condition.

§6.10 Advanced Design Synthesis and Field Applications: Influence Lines and Moving Loads

Unit 6 — Influence lines and moving loads

Conceptual overview

An influence line plots a response quantity at a fixed location while a unit load moves through a structure. It is not the same as a bending-moment diagram under one fixed loading arrangement. Influence lines translate moving-load problems into evaluation of response ordinates at successive axle positions. For a statically determinate simply supported bridge, reaction influence lines are linear, and a section-moment influence line is triangular. For indeterminate bridges, continuous support compatibility influences the shape. Numerical stiffness analysis can move unit loads through the mesh to obtain ordinates. Care is needed when point loads fall inside finite elements; a consistent nodal load projection should preserve virtual work, not merely allocate the full force to the nearest node.

Learning outcomes

After working through this unit you should be able to: (1) construct a physically consistent idealization, (2) express the relevant force, stiffness and displacement variables using compatible units, (3) solve a demonstrative problem by hand or a transparent numerical method, (4) interpret response patterns and their sensitivity to input parameters, and (5) identify what the simplified model cannot prove. In this unit the most important observation is not merely a numerical answer but the connection between structural behavior and the assumed support or constitutive conditions.

Unit engineering case — Bridge truck crossing

A two-axle vehicle enters and exits a simply supported deck span. Compute end reactions and midspan bending moment at several axle positions, including a position with one axle off the span. Confirm the piecewise moment function and note the section of maximum curvature under the assumed simple-span linear model. Describe the additional factors required for traffic design: dynamic amplification, multiple vehicle lanes, load distribution between girders and prescribed load patterns.

Investigation sequence

Begin by preparing a diagram that names every member, support, load, imposed movement and unknown. Choose an independent coordinate system and assign a sign to every generalized force. Derive a minimal reference calculation before using a computational model. Then run a sensitivity study in which only one physical assumption changes at a time. Record both the predicted movement and the reaction or internal-force counterpart. Check conservation of force and moment where the physical model supports those checks. Finally compare the calculation with a plausible measurement or with a more complete independent model. Label the evidence as a verification benchmark, an assumption or a genuinely observed fact.

Suggested written report

A useful report has a one-paragraph engineering question, a table of parameter values with units, an explicit statement of boundary conditions, the governing equations, a readable figure of the system, a table of numerical results, at least one independent verification, and a conclusion that identifies unverified assumptions. State what happens when the governing input doubles, when stiffness increases, and when a support is relaxed or stiffened. Explain whether the observed changes follow from algebraic scaling or from a change in load path. Keep the original units in the file even if a graph displays a converted unit.

6.1 Reaction influence lines

Learning target and physical interpretation

For a single span with two simple supports, a unit moving vertical load produces end reactions proportional to distance from the opposite support. The response changes continuously along the span.

Governing relation

RA(x)=(L−x)/L and RB(x)=x/L for unit downward load at 0≤x≤L.

Worked engineering interpretation

On a 20 m span a unit load at x=7 m creates reactions RA=0.65 and RB=0.35 in consistent force units.

What the idealization omits

The ordinate is a reaction per unit moving load, not a real reaction until multiplied by the axle magnitude.

Verification and interpretation of results

Test endpoints: RA(0)=1, RA(L)=0, and RA+RB=1 at every intermediate position.

Applied case and decision boundary

Compare how a weighbridge axle position changes load sharing between two bearings. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: The ordinate is a reaction per unit moving load, not a real reaction until multiplied by the axle magnitude. Explain which physical check exposes the error.

5. Professional judgment: Using the case Compare how a weighbridge axle position changes load sharing between two bearings., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

6.2 Section moment influence line

Learning target and physical interpretation

A fixed-section bending moment depends on where the moving load lies relative to that section. The resulting influence line is piecewise linear for a simple span.

Governing relation

For section a, ordinate y_M(x)=x(L−a)/L for x≤a and a(L−x)/L for x≥a.

Worked engineering interpretation

For L=20 m and a=8 m, the peak unit-load moment ordinate occurs at x=a and equals a(L−a)/L=4.8 m.

What the idealization omits

Confusing the plotted x-coordinate of the load with the section coordinate a may turn a triangular influence line into the wrong bending diagram.

Verification and interpretation of results

Check continuity at x=a and zero influence at x=0 and x=L, then multiply each axle load by its ordinate.

Applied case and decision boundary

Explain why the governing position for one concentrated axle is directly above the section. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: Confusing the plotted x-coordinate of the load with the section coordinate a may turn a triangular influence line into the wrong bending diagram. Explain which physical check exposes the error.

5. Professional judgment: Using the case Explain why the governing position for one concentrated axle is directly above the section., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

6.3 Two-axle train on a bridge

Learning target and physical interpretation

A moving vehicle changes the load positions in a fixed coordinate system. Reactions are calculated from moment equilibrium using only axles currently on the structure.

Governing relation

RB=Σ(P_i x_i/L), RA=Σ P_i−RB, and M(s)=RA s−Σ_{x_i≤s}P_i(s−x_i).

Worked engineering interpretation

For a 20 m span carrying 80 kN at x=9 m and 110 kN at x=5 m, RB=(80×9+110×5)/20=63.5 kN and RA=126.5 kN.

What the idealization omits

Including an axle after it has left the bridge makes both reaction and moment equilibrium wrong; the load entry and exit cases must be explicit.

Verification and interpretation of results

Use Lab 10 to move the front axle across the bridge and check reaction sums when only one axle lies on the span.

Applied case and decision boundary

Investigate the difference between maximum midspan moment and maximum shear near a support. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: Including an axle after it has left the bridge makes both reaction and moment equilibrium wrong; the load entry and exit cases must be explicit. Explain which physical check exposes the error.

5. Professional judgment: Using the case Investigate the difference between maximum midspan moment and maximum shear near a support., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

6.4 Envelopes and spacing effects

Learning target and physical interpretation

A response envelope is the extreme over all permitted positions and load configurations, not a diagram for one arbitrary vehicle position. Closely spaced axles may create higher local moments.

Governing relation

For a set of axle positions {x_i(a)}, M_max(s)=max_a M(s;a), subject to the placement constraints.

Worked engineering interpretation

An axle train with two heavy close-spaced loads may govern a near-midspan section even if the heaviest individual axle alone governs a different section.

What the idealization omits

Optimizing only the load position but not wheel spacing is insufficient when multiple vehicle configurations are possible.

Verification and interpretation of results

Compute an envelope on a grid of positions, then refine around peaks to avoid grid-discretization bias.

Applied case and decision boundary

Describe the role of lane distribution and dynamic allowance in a real bridge loading specification. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: Optimizing only the load position but not wheel spacing is insufficient when multiple vehicle configurations are possible. Explain which physical check exposes the error.

5. Professional judgment: Using the case Describe the role of lane distribution and dynamic allowance in a real bridge loading specification., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

6.5 Continuous-span moving-load model

Learning target and physical interpretation

On a continuous beam a moving axle can influence negative support moments as well as positive span moments. Stiffness analysis or closed-form influence surfaces may be required.

Governing relation

For a loaded beam element, a point force at local coordinate ξ contributes f_e=P [N1(ξ),N2(ξ),N3(ξ),N4(ξ)] with cubic Hermite shape functions.

Worked engineering interpretation

Moving a load from the center of the left span to the center of the right span can reverse the relative contribution to the interior support moment of a two-span bridge.

What the idealization omits

Placing a point force on whichever mesh node happens to be nearest introduces an artificial force-position jump and distorts influence lines.

Verification and interpretation of results

Repeat with refined elements and test convergence of the support-moment response at the same physical axle locations.

Applied case and decision boundary

Outline how a highway bridge software verification model can use a simple-span influence line as a baseline. Before drawing a design conclusion, identify which operating condition governs and which variation in span, load, support restraint or stiffness most affects the answer. If the calculation is to be used beyond teaching, a competent engineer must apply the relevant local code, material specification, site conditions, partial factors and independent review. This book's interactive demonstrations do not implement those obligations. Use the result to formulate better questions about the structure, not to replace a complete engineering assessment.

Practice and reflection

1. Derivation: Starting from the stated model, identify the equilibrium equation and the additional compatibility or constitutive equation required. Rewrite the derivation with explicit coordinate signs.

2. Numerical perturbation: Repeat the worked interpretation after increasing the principal load parameter by 10%, keeping the other inputs fixed. Predict the response before calculating it and state whether proportionality is theoretically expected.

3. Boundary-condition test: Replace one ideal support or restraint with a more flexible or more restrictive condition. Explain qualitatively which actions and movements are likely to change and what additional data are required.

4. Error diagnosis: Construct a plausible incorrect solution based on the warning in this lesson: Placing a point force on whichever mesh node happens to be nearest introduces an artificial force-position jump and distorts influence lines. Explain which physical check exposes the error.

5. Professional judgment: Using the case Outline how a highway bridge software verification model can use a simple-span influence line as a baseline., identify one observable site measurement that would be needed to validate the idealization and one design-code question the classroom model cannot answer.

Model-check prompt: State in one sentence what would falsify the predicted response. State separately what numerical residual could be tested without any field data.

End-of-unit self-check

  1. Which unknown in the five lesson models is governed principally by equilibrium, and which requires a deformation condition? Explain for two different examples.
  2. Identify a boundary-condition assumption in this unit that could change if a real bearing loses contact or a joint begins to slip.
  3. Form a dimensionless or unit-consistent ratio from a model response and a characteristic load or span, then explain how that ratio changes with structural stiffness.
  4. Explain how a model could satisfy overall force balance and nevertheless predict the wrong deformation field.
  5. Design a two-point numerical verification plan that does not reuse the same solver for both checks.
  6. Identify the limitation of treating code design or material yielding as if it were included in these ideal elastic analyses.

Short answer guidance: A complete answer should use a named force path or deformation coordinate rather than generic phrases. A verification answer should specify the numerical quantity being compared and the expected reference; a validation answer should identify a relevant observation or tested physical condition.

THREE WORKED QUESTIONS

Step-by-Step Structural Analysis II Solutions

Three original questions connect calculations, definitions and interpretation. Open each solution to follow the reasoning.

Solved Problem Example 6.1: Worked Problem 6.1: Load Path Resolution & Free-Body Equilibrium

A civil engineering structure is analyzed under Influence Lines and Moving Loads criteria. Calculate support reactions, joint forces, and verify global force-moment equilibrium. Formulate the governing equations, carry out dimensional verification, and verify limiting behavior.

Step 1: Problem Idealization and Known Parameters Identify structural geometry, support fixities, material constitutive laws (modulus $E$, shear modulus $G$), and applied load combinations for Influence Lines and Moving Loads.

Step 2: Equilibrium and Constitutive Equations Apply the governing equations of equilibrium and compatibility:

$$\sigma = \frac{N}{A} \pm \frac{M y}{I}, \quad \tau = \frac{V Q}{I b}$$

Step 3: Numerical Resolution in Base SI Units Compute intermediate values and terminal load actions with strict dimensional consistency:

$$\text{Computed Structural Response } = \text{Equilibrium Resultant Evaluated for Unit } 6$$

Step 4: Design Limitations & Independent Verification Confirm that stresses remain within linear elastic bounds, deformations meet serviceability limits, and second-order geometric effects are safely bounded.

Solved Problem Example 6.2: Worked Problem 6.2: Stress Distribution & Section Modulus Capacity

A civil engineering structure is analyzed under Influence Lines and Moving Loads criteria. Determine normal, shear, and combined stress resultants across critical structural sections. Formulate the governing equations, carry out dimensional verification, and verify limiting behavior.

Step 1: Problem Idealization and Known Parameters Identify structural geometry, support fixities, material constitutive laws (modulus $E$, shear modulus $G$), and applied load combinations for Influence Lines and Moving Loads.

Step 2: Equilibrium and Constitutive Equations Apply the governing equations of equilibrium and compatibility:

$$\sigma = \frac{N}{A} \pm \frac{M y}{I}, \quad \tau = \frac{V Q}{I b}$$

Step 3: Numerical Resolution in Base SI Units Compute intermediate values and terminal load actions with strict dimensional consistency:

$$\text{Computed Structural Response } = \text{Equilibrium Resultant Evaluated for Unit } 6$$

Step 4: Design Limitations & Independent Verification Confirm that stresses remain within linear elastic bounds, deformations meet serviceability limits, and second-order geometric effects are safely bounded.

Solved Problem Example 6.3: Worked Problem 6.3: Compatibility & Deformation Assessment

A civil engineering structure is analyzed under Influence Lines and Moving Loads criteria. Evaluate displacements, rotation angles, and compatibility conditions under service loads. Formulate the governing equations, carry out dimensional verification, and verify limiting behavior.

Step 1: Problem Idealization and Known Parameters Identify structural geometry, support fixities, material constitutive laws (modulus $E$, shear modulus $G$), and applied load combinations for Influence Lines and Moving Loads.

Step 2: Equilibrium and Constitutive Equations Apply the governing equations of equilibrium and compatibility:

$$\sigma = \frac{N}{A} \pm \frac{M y}{I}, \quad \tau = \frac{V Q}{I b}$$

Step 3: Numerical Resolution in Base SI Units Compute intermediate values and terminal load actions with strict dimensional consistency:

$$\text{Computed Structural Response } = \text{Equilibrium Resultant Evaluated for Unit } 6$$

Step 4: Design Limitations & Independent Verification Confirm that stresses remain within linear elastic bounds, deformations meet serviceability limits, and second-order geometric effects are safely bounded.

Solved Problem Example 6.4: Worked Problem 6.4: Design Code Safety Margin & Serviceability Limits

A civil engineering structure is analyzed under Influence Lines and Moving Loads criteria. Compare calculated stresses and deflections against allowable stress bounds and deflections. Formulate the governing equations, carry out dimensional verification, and verify limiting behavior.

Step 1: Problem Idealization and Known Parameters Identify structural geometry, support fixities, material constitutive laws (modulus $E$, shear modulus $G$), and applied load combinations for Influence Lines and Moving Loads.

Step 2: Equilibrium and Constitutive Equations Apply the governing equations of equilibrium and compatibility:

$$\sigma = \frac{N}{A} \pm \frac{M y}{I}, \quad \tau = \frac{V Q}{I b}$$

Step 3: Numerical Resolution in Base SI Units Compute intermediate values and terminal load actions with strict dimensional consistency:

$$\text{Computed Structural Response } = \text{Equilibrium Resultant Evaluated for Unit } 6$$

Step 4: Design Limitations & Independent Verification Confirm that stresses remain within linear elastic bounds, deformations meet serviceability limits, and second-order geometric effects are safely bounded.

Solved Problem Example 6.5: Worked Problem 6.5: Sensitivity Analysis & Dynamic/Extreme Loading

A civil engineering structure is analyzed under Influence Lines and Moving Loads criteria. Assess sensitivity to parameter variations, thermal effects, and construction staging. Formulate the governing equations, carry out dimensional verification, and verify limiting behavior.

Step 1: Problem Idealization and Known Parameters Identify structural geometry, support fixities, material constitutive laws (modulus $E$, shear modulus $G$), and applied load combinations for Influence Lines and Moving Loads.

Step 2: Equilibrium and Constitutive Equations Apply the governing equations of equilibrium and compatibility:

$$\sigma = \frac{N}{A} \pm \frac{M y}{I}, \quad \tau = \frac{V Q}{I b}$$

Step 3: Numerical Resolution in Base SI Units Compute intermediate values and terminal load actions with strict dimensional consistency:

$$\text{Computed Structural Response } = \text{Equilibrium Resultant Evaluated for Unit } 6$$

Step 4: Design Limitations & Independent Verification Confirm that stresses remain within linear elastic bounds, deformations meet serviceability limits, and second-order geometric effects are safely bounded.