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Linear static analysis

The workhorse analysis — what K u = f actually assumes, what it returns, and where linearity stops being a reasonable model.

Analysis types 2 min read

Linear static analysis solves

for the displacement vector , given the assembled stiffness matrix and the load vector . Internal forces, stresses and reactions are all recovered from .

What "linear" is promising

Three separate assumptions travel under that one word:

AssumptionMeansFails when
Material linearityStress proportional to strain, no yieldSteel yields, concrete cracks, timber creeps
Geometric linearityEquilibrium written on the undeformed shapeSlender frames sway, cables change geometry
Boundary linearityRestraints do not change with loadFoundations lift off, gaps close, friction slips

All three hold in most everyday design. Know which one you are relying on.

What you get back

  • Displacements — translations and rotations at nodes, interpolated along members.
  • Internal forces — , , , , , along beams and bars; moments and membrane forces in surfaces.
  • Reactions — at every restrained degree of freedom.
  • Stresses — derived from internal forces and section properties.

Superposition

Because the system is linear, the response to a combination equals the factored sum of the responses to its cases:

In practice:

  • Each load case is solved once, all of them in one pass.
  • Every combination is a factored sum of the load-case results; nothing is solved again.
  • Fifty combinations cost barely more than one.

Reading the result

Deflected shape, then equilibrium, then one hand check, then the governing numbers with their combinations. The order matters, and it is written out once in Troubleshooting.

Drag the load in the demo below and watch reactions, moment and deflection follow: the same quantities, in the same order, you read off a real model.

24.0 kN16.0 kNP = 40 kNa = 2.40 mb = 3.60 m M = 57.6 kNm My
Max. moment
57.6 kNm
Max. deflection
9.7 mm · L/617
Reactions
24.0 / 16.0 kN
Bending · §6.2.5
η = 0.39 OK
IPE 300 · S235 · span 6 m · γM0 = 1.0
Point load only, self-weight ignored.
Deflected shape drawn ×40.

Deflection limits

Deflection is checked at SLS, not ULS, and against the correct combination for what is being protected — see Automatic combinations. Common limits:

SituationTypical limit
Beams, total deflectionspan / 250
Beams supporting brittle finishesspan / 500 after finishes
Cantileverslength / 180
Inter-storey drift, no brittle claddingheight / 300

These are indicative. The applicable limit comes from the code, the national annex and the project specification, each overriding the one before. Members can be checked against the tabulated limits automatically, each on its own combination, with a serviceability check; slabs are read off the contour.

Where linear static is not enough

SituationWhat to do
Slender sway frameCheck with linear buckling, then run a second-order analysis
Foundation upliftLook at spring forces; interpret by hand where tension appears
Cracked concrete deflectionUse the code's cracked-section method; the linear result is uncracked
Vibration and dynamicsModal analysis
Post-yield behaviourNot in this release; material nonlinearity is on the roadmap

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