Langford Analytic · Knowledge Base

Engineering Load Types & Load Cases Fundamentals

How forces, moments, pressure, acceleration, temperature and imposed motion become structural loading.

Article 34Fundamentals12 min read
loadsforcemomentpressureaccelerationthermalfundamentals

What Is It?

A load is any external action or imposed condition that causes a structure to develop internal force, stress, strain, deformation or dynamic response. Loads are the inputs to structural analysis — before stress, displacement or margin can be assessed, the engineer must understand what loads act, where they act, when they act, how they combine and how the structure reacts. Loads may be forces, moments, pressures, accelerations, thermal strains, imposed displacements, preloads or contact loads. Each has a physical origin, a magnitude, a direction, a distribution and a timing. The discipline of loads engineering is the practice of defining these inputs rigorously and defensibly.

Why It Matters

If the loads are wrong, the analysis is wrong. No amount of modelling sophistication, mesh refinement or computational power can repair an incorrect load set. A beautifully constructed finite element model driven by the wrong loads produces beautifully presented wrong answers. The loads definition is the first and most consequential step in structural analysis — it determines what the structure is being asked to carry, and therefore what the analysis is actually assessing. Understanding loads at a fundamental level is essential for every structural analyst, stress engineer and loads engineer.

A load is not just a number. It has magnitude, direction, location, distribution and physical origin. A load without these attributes is incomplete — and an incomplete load definition is a source of engineering error.

Load Types

Load TypePhysical OriginUnitsStructural Effect
ForceMechanical action; contact; inertia; gravityNStress; deformation; reaction
MomentForce at a distance; couple; torsionN·mBending stress; torsional stress
PressureFluid or distributed contact over an areaPa (N/m²)Membrane stress; bending; local stress
Distributed loadForce per unit length or areaN/m or N/m²Shear; bending; local response
AccelerationChange in velocity; rotational motionm/s² or rad/s²Inertial force through mass
Thermal strainTemperature change with restraintΔT (K)Thermal stress; deformation
Imposed displacementSettlement; interference; preloadmmReaction force; stress without applied force
PreloadAssembly; bolt torque; press fitNInitial stress; contact pressure
Contact loadSurface interaction between bodiesNLocal contact stress; pressure distribution

The Load Is Not Just a Number

A common mistake is to treat a load as a single scalar value. "The load is 50 kN" is incomplete — it does not say where the load acts, in what direction, over what area, or what produces it. A complete load definition specifies all of these attributes. The magnitude is the size of the load. The direction is the vector along which it acts. The location is the point or region where it is applied. The distribution describes how the load is spread over the application region. The physical origin explains what creates the load — a contact force, an aerodynamic pressure, an inertial acceleration, a thermal expansion. Without all five, the load definition is ambiguous and the analysis is not reproducible.

THE LOAD IS NOT JUST A NUMBER — IT HAS MAGNITUDE, DIRECTION, LOCATION AND PHYSICAL ORIGIN. Every load in a structural model should be traceable to its physical origin. A load without a physical origin is a guess, not a definition.

External vs Internal Load

External loads are the forces, moments, pressures and conditions applied to the structure from outside — aerodynamic pressure, contact forces, gravity, thermal environment, imposed displacement. Internal loads are the forces and moments that develop within the structure in response to the external loads — shear, bending, torsion, axial force, stress. The external load is the input; the internal load is the response. The structural analysis converts the external loads into internal loads through the structural model. Understanding the distinction is essential: the engineer defines the external loads and the analysis computes the internal loads. Confusing the two — applying an internal load as if it were external, or vice versa — leads to incorrect analysis.

Global, Local, Interface and Reaction Load

Loads exist at different structural scales. The global load is the overall load system acting on the complete structure — the total lift, the total weight, the total thrust. The local load is the load at a specific point or region — the load at a fastener, the pressure at a panel, the force at a fitting. The interface load is the load transferred between two components or subsystems — the load from a wing to a fuselage, the load from a bracket to a beam. The reaction load is the force and moment generated at the supports to maintain equilibrium. Each scale has its own analysis and its own verification. The global load must balance; the local load must be compatible with the local structure; the interface load must be transferred correctly between models; the reaction must equal the applied load.

Static vs Dynamic Loading

Static loading is a load that is applied slowly and remains constant or changes slowly enough that inertia effects are negligible. The structural response is governed by stiffness and strength, not by mass or damping. Dynamic loading is a load that changes rapidly enough that inertia and damping effects are significant — the structural response depends on the mass distribution, the natural frequencies and the load timing. Dynamic loads include vibration, shock, impact and transient events. The distinction is critical because a static analysis of a dynamically loaded structure misses the dynamic amplification, the resonance and the transient response. Conversely, a dynamic analysis of a statically loaded structure is unnecessary complexity.

AspectStatic LoadingDynamic Loading
Load rateSlow; constant or slowly varyingRapid; transient; oscillatory
Inertia effectsNegligibleSignificant; governs response
Response depends onStiffness and strengthMass, stiffness, damping, frequency
Analysis typeStatic; quasi-staticModal; harmonic; transient; spectral
Typical examplesSelf-weight; steady pressure; bolt preloadVibration; shock; impact; gust; acoustic

Concentrated vs Distributed Loading

A concentrated load (point load) is a force applied at a single point. In reality, no load is truly at a point — even a sharp contact has a finite area — but the point-load approximation is useful when the application area is small compared to the structural dimension. A distributed load is a force spread over a length, area or volume. Pressure is a distributed load per unit area. A body force is a distributed load per unit volume (gravity, inertia). The same total force can produce very different structural responses depending on whether it is concentrated or distributed and on the distribution pattern. A concentrated load creates high local stress; the same total load distributed over a wide area creates lower stress but may produce significant bending.

Common Mistakes

COMMON MISTAKE: Treating a load as a single number without specifying its direction, location, distribution and physical origin. A load defined only by magnitude is ambiguous and leads to analysis that cannot be reproduced or verified.

Verification

LOAD CHECK: For every load in the structural model, confirm that its magnitude, direction, location, distribution and physical origin are documented. If any attribute is missing, the load definition is incomplete.

Key Takeaways

  • A load is any external action or imposed condition that causes structural response
  • Every load has magnitude, direction, location, distribution and physical origin
  • External loads are inputs; internal loads are the structural response
  • Loads exist at global, local, interface and reaction scales
  • The static/dynamic and concentrated/distributed distinctions determine the analysis approach