GLOBAL KNOWLEDGE ARK

Engineering & Technology · Civil Structures & Structural Engineering

Structural analysis, deformation, stability and serviceability

Two beams can have the same load reactions yet different deflections. A member can remain below a material stress limit and still become unstable, or move enough to impair its use. Structural analysis needs several questions to be answered together rather than one reassuring stress value.

Use Statics & Solid Mechanics, Materials Selection & Degradation and Measurement, Units & Engineering Evidence. Floor pressures, member properties, oscillator inputs and remaining areas are hypothetical teaching assumptions. No site-specific hazards, current code values, construction permissions or qualified structural designs are supplied.

Back to the chapter

After reading, you can

Distinguish equilibrium, deformation compatibility, constitutive response, stability and serviceability in a structural model.

01

Combine the three ingredients of an elastic analysis

Equilibrium relates external loads to reactions and internal actions. Compatibility requires connected deformations to fit the restraints and each other. A constitutive relation connects force or stress to deformation, such as an assumed elastic modulus. In a statically determinate model, equilibrium can determine reactions directly; redundant supports usually require deformation information as well.

Choose degrees of freedom and boundary conditions deliberately. A simple support restrains specified motion while permitting rotation in the idealization. A fixed end restrains rotation as well. Actual connections have finite stiffness and can slip. A calculation using the wrong support model may be internally consistent while predicting the wrong force distribution.

02

Separate stiffness from strength and usability

Flexural rigidity EI combines material modulus E with the cross-section’s second moment of area I. Under small-rotation, slender-beam assumptions, moment is related to curvature through EI. Integrating with appropriate boundary conditions gives deflection. This model omits effects such as large rotations, significant shear deformation or changing cracked stiffness unless they are added explicitly.

Serviceability concerns performance during use: deflection can disturb partitions or drainage, and vibration can affect occupants or equipment. These requirements are separate from resistance to collapse. An applicable criterion and operating condition must be supplied before a deflection can be called acceptable. A magnitude alone does not establish a pass or failure.

Strength, stiffness and stability answer different questionsAn original elastic beam calculation plots downward deflection magnitude with an upward numerical axis.A stiffness change affects deflection under the same loadDownward deflection magnitude / mmPosition along a simply supported 6 m beam / m01234560123456Solid: EI = 6 MN m²; dashed: EI = 12 MN m²; w = 2 kN/mMagnitude graph, not a scale drawing of the bent beam; supports at x=0 and x=6
Uniform load 2 kN/m, span 6 m, constant flexural rigidity EI=6 MN m². Downward deflection magnitude v(x)=w x(L³−2 Lx²+x³)/(24 EI), with consistent metre/newton units. It vanishes at both simple supports and reaches 5.625 mm at midspan. Doubling EI halves the plotted magnitude to 2.8125 mm. Positive values are downward magnitudes plotted upward on a numerical axis, not a physical shape. Load reactions 6 kN each and maximum moment 9 kN m are unchanged in this determinate model.
03

Ask whether the equilibrium remains stable

A compressed member’s lateral displacement can add moment because its axial force now acts through an offset. This geometric effect is often called a second-order effect. A perfectly straight elastic pin-ended column has ideal Euler critical force π²EI/L². End restraint, imperfections, material nonlinearity and local buckling change what that model can establish for a real member.

Computer models assemble equilibrium and compatibility over many elements. Refine a mesh to examine numerical convergence, but also examine restraints, load introduction and material assumptions. Two meshes can converge to nearly the same result for an unsuitable physical model. Check reactions, units, deformed shape and a simpler limiting case before trusting a visually detailed contour plot.

One load account, two bending stiffnesses

Supply a simply supported 6 m beam with uniform line load 2 kN/m and constant EI=6 MN m². Reactions are 6 kN each and the maximum bending moment is wL²/8=9 kN m. The slender linear beam model gives maximum downward deflection 5 wL⁴/(384 EI)=0.005625 m, or 5.625 mm.

The plotted function is v(x)=w x(L³−2 Lx²+x³)/(24 EI), the downward magnitude for x in metres and consistent newton units. It is zero at both ends. Doubling EI gives 2.8125 mm at midspan but leaves the reactions and moments unchanged in this determinate case. No allowable deflection or strength has been supplied, so neither beam is qualified by this comparison.

Try the reasoning

  1. If an ideal pin-ended column’s length doubles with EI unchanged, what happens to its Euler critical force?

    Show the answer and reasoning

    It becomes one-quarter because the ideal expression varies with 1/L². That scaling is not a real-column capacity approval.

  2. An axial force of 100 kN acts through a 10 mm lateral offset. What additional moment magnitude results?

    Show the answer and reasoning

    Pδ=100×0.010=1 kN m. A second-order analysis must account for how that offset itself changes under load.

  3. Does a mesh change below 1% prove a correct support assumption?

    Show the answer and reasoning

    No. It indicates limited numerical sensitivity for that chosen model, not physical validation of its restraints.

What to carry forward

Check equilibrium, deformation, stability and use separately, and connect each result to the assumptions that produced it.

References

Teaching resources and research supporting this lesson’s explanations and examples.

  1. Massachusetts Institute of Technology3 sources
    1. Engineering Mechanics for Structures, Chapter 2: Equilibrium (2004)Louis L. Bucciarelli · MIT 1.050Primary teaching or institutional technical source · PDFocw.mit.eduRead source
    2. Building Structural Systems II: Steel (2002), selected conceptual slidesJohn Ochsendorf · MIT 4.463Primary teaching or institutional technical source · PDFocw.mit.eduRead source
    3. Engineering Mechanics for Structures, Chapter 10: Deflections due to Bending (2004)Louis L. Bucciarelli · MIT 1.050Primary teaching or institutional technical source · PDFocw.mit.eduRead source