Ubicación: Global + English
Global Global Algérie Français Algeria English Angola Português Angola English Argentina Español Argentina English Australia English Austria Deutsch Austria English Azerbaijan English Azerbaijan Русский Bahrain English Bangladesh English Belgium English Belgium Français Belgium Nederlands Brazil Português Brazil English Bulgaria български Bulgaria English Cameroon English Cameroon Français Canada English Canada Français Chile Español Chile English China 中文 China 日本語 China English Colombia Español Colombia English Croatia English Czech Republic Čeština Czech Republic English Denmark English Djibouti English Ecuador Español Ecuador English Egypt English Estonia English Ethiopia English Finland Suomi Finland English France Français France English Georgia English Georgia Русский Germany Deutsch Germany English Ghana English Greece Ελληνικά Greece English Guatemala Español Guatemala English Hong Kong, China English Hong Kong, China 中文 Hungary Magyar Hungary English India English Indonesia English Iraq English Ireland English Italy Italiano Italy English Ivory Coast Français Ivory Coast English Japan 日本語 Japan English Jordan English Kazakhstan Русский Kazakhstan English Kenya English Kuwait English Kyrgyzstan Русский Kyrgyzstan English Latvia English Lithuania English Malaysia English Mauritius English Mauritius français (Maurice) Mexico Español Mexico English Moldova Română Moldova English Mongolia English Morocco English Morocco Français Mozambique Português Mozambique English Netherlands Nederlands Netherlands English New Zealand English Nigeria English Norway English Oman English Pakistan English Paraguay Español Paraguay English Peru Español Peru English Philippines English Poland Polski Poland English Portugal Português Portugal English Qatar English Republic of Korea 한국어 Republic of Korea English Romania Română Romania English Saudi Arabia English Serbia Српски Serbia English Singapore English Slovakia English Slovenia English South Africa English Spain English Spain Español Sri Lanka English Sweden English Switzerland Deutsch Switzerland Français Switzerland Italiano Switzerland English Tanzania English Thailand ไทย Thailand English Togo English Togo Français Tunisia English Tunisia Français Türkiye Türkçe Türkiye English Turkmenistan Русский Turkmenistan English Ukraine Українська Ukraine English United Arab Emirates English United Kingdom English Uruguay Español Uruguay English USA English Uzbekistan English Uzbekistan Русский Vietnam Tiếng Việt Vietnam English

Dynamic compression fatigue strain-controlled testing evaluates how materials withstand repeated compressive cyclic loading when strain amplitude, rather than force, is maintained as the controlled variable throughout the test. This method is essential for characterizing fatigue life, cyclic stress response, heat build-up, and permanent set in rubbers, elastomers, polymer foams, and metallic alloys. This article explains the underlying principles, specimen types, measured parameters, standard test procedures, and typical industrial applications of this important fatigue evaluation technique.

Technical Overview

Dynamic compression fatigue strain-controlled testing is a laboratory technique in which a specimen is subjected to a cyclically varying compressive deformation while the testing machine regulates the strain amplitude, waveform shape, and cycling frequency as the primary controlled variables. Because the imposed deformation is fixed while the material response is free to evolve, this method closely reproduces the service conditions of components whose deflection is dictated by geometry or assembly constraints, such as vibration mounts, cushioning layers, seals, and clearance-limited structural members.

During cyclic compression, viscoelastic and elastoplastic materials exhibit hysteresis, meaning that a portion of the mechanical energy input in each cycle is dissipated as heat or accumulated as microstructural damage. As cycling proceeds, the measured compressive stress typically decreases due to cyclic softening, stress relaxation, or crack initiation and growth. Recording the evolution of peak stress, hysteresis loop shape, surface temperature, and residual deformation allows engineers to quantify degradation kinetics and to define a statistically meaningful fatigue life.

Relevant reference standards and guidelines for strain-controlled and compression fatigue testing include the following:

  • ASTM D623 — Standard Test Methods for Rubber Property: Heat Generation and Flexing Fatigue in Compression
  • ASTM E606/E606M — Standard Test Method for Strain-Controlled Fatigue Testing of metallic materials
  • ISO 12106 — Metallic materials: Fatigue testing: Axial-strain-controlled method
  • GB/T 15248 — Axial strain-controlled fatigue testing method for metallic materials
  • ASTM E467 — Verification of constant-amplitude dynamic loads on fatigue testing systems, used for machine qualification

Testing Samples

Vulcanized Rubber and Thermoplastic Elastomer Compounds

Compression-molded cylindrical buttons or disk specimens are the most common geometry for rubbery materials. Standard cylindrical specimens, typically on the order of 17 to 25 mm in diameter with a height-to-diameter ratio close to unity, are bonded or clamped between parallel platens so that bulging is constrained and the deformation state remains predominantly uniaxial compression. Compound formulation, cure state, and surface finish must be documented because all three strongly influence fatigue performance.

Polymer Foams and Cellular Cushioning Materials

Flexible and semi-rigid foams, such as polyurethane, EVA, and PE foams used in footwear midsoles, padding, and packaging, are tested as rectangular or cylindrical blocks with planar, parallel faces. Specimen height is selected so that the imposed strain amplitude remains within the usable compressive range of the cellular structure, and preconditioning cycles are usually applied to stabilize the initial viscoelastic response before formal data collection begins.

Metallic Alloys

For strain-controlled low-cycle fatigue evaluation of metals, cylindrical specimens with a uniform gauge section or hourglass profile are machined per ASTM E606/E606M and ISO 12106. When compression loading is involved, antibuckling guides or a reduced gauge length may be employed to prevent lateral instability while preserving valid strain measurement.

Component-Level Elastomeric Articles

Finished products, including engine mounts, bushings, gaskets, diaphragms, and elastomeric bridge bearing pads, can be tested in dedicated fixtures that reproduce the actual boundary conditions. Component-level testing complements material-level data by capturing the influence of geometry, bonding, and load-transfer interfaces on fatigue durability.

Testing Items

The principal quantities determined in a dynamic compression fatigue strain-controlled experiment include:

  • Fatigue life, expressed as the number of cycles to a defined failure criterion at a given strain amplitude and strain ratio
  • Cyclic stress response, including the evolution of peak compressive stress, stress amplitude, and mean stress with accumulated cycles
  • Hysteresis loop area and energy dissipated per cycle, which indicate damping capacity and heat generation potential
  • Dynamic stiffness and complex modulus, including storage modulus, loss modulus, and loss factor derived from the stress-strain ellipse
  • Heat build-up, measured as the temperature rise of the specimen surface or core during continuous cycling
  • Permanent set and residual deformation, evaluated by interrupting or completing the test and measuring unrecovered height
  • Softening ratio, defined as the percentage reduction in peak stress relative to the initial cycle
  • Failure morphology, including crack initiation sites, crack growth paths, and internal heat-induced degradation
  • Strain-life (epsilon-N) curves and cyclic stress-strain curves constructed from replicate tests at multiple strain amplitudes

Testing Methods

Apparatus and Instrumentation

Testing is performed on servo-hydraulic or electrodynamic universal testing machines equipped with compression platens, a calibrated load cell, and a strain measurement device. Strain may be measured or commanded through a crosshead displacement transducer, a contact extensometer attached to the gauge section, or, for soft materials, a laser or video extensometer. Infrared thermography or embedded fine-gauge thermocouples monitor temperature rise, and environmental chambers allow testing at elevated, subambient, or humidity-controlled conditions when required by the specification.

Specimen Preparation and Conditioning

Specimens are machined, molded, or die-cut to the specified geometry, and dimensions are verified at multiple locations. Metallic specimens are polished in the gauge section to remove machining marks that could act as crack initiation sites. Elastomeric and foam specimens are conditioned at standard laboratory temperature and humidity, typically 23 degrees Celsius and 50 percent relative humidity, for a defined period before testing to ensure reproducible viscoelastic state.

Test Parameter Configuration

The test program defines the mean strain, strain amplitude, waveform, frequency, and strain ratio R, calculated as the ratio of minimum to maximum strain. Fully compressive cycling, where R is greater than zero, is customary for cushioning and mounting applications. Frequencies are selected to balance test duration against self-heating; rubber and foam testing is often conducted between 1 and 30 Hz, while metallic strain-controlled tests commonly operate at 0.1 to 5 Hz. A series of progressively increasing preconditioning cycles may be applied to seat the specimen and stabilize the fixture before zeroing the strain reference.

Data Acquisition and Failure Criteria

Complete hysteresis loops are captured at logarithmic cycle intervals, for example at cycle 1, 10, 100, and every subsequent decade, along with continuous records of peak stress and temperature. Failure is typically defined by one or more of the following criteria: a specified drop in peak compressive stress, commonly 10 to 50 percent depending on the material class; visible cracking or rupture; a limiting temperature rise; or complete specimen collapse. Testing is terminated at a run-out limit, frequently 1 to 10 million cycles, if failure has not occurred. The final report documents the loading parameters, environmental conditions, cycles to failure, stress and temperature histories, and post-test residual deformation measurements.

Applications

Dynamic compression fatigue strain-controlled testing supports material qualification, design validation, and lifetime prediction across many industries:

  • Automotive engineering: durability assessment of engine mounts, suspension bushings, vibration isolators, tire compounds, and NVH components subjected to millions of road-induced compression cycles
  • Footwear and sporting goods: evaluation of EVA and PU midsole cushioning retention and fatigue-induced compression set
  • Sealing technology: verification of gasket and O-ring performance under cyclic closure and thermal-mechanical loading
  • Infrastructure: qualification of elastomeric bridge bearings and seismic isolation pads under long-term cyclic compression
  • Energy and electronics: characterization of battery cushion pads, foam spacers, and potting compounds in vibration-exposed assemblies
  • Biomedical devices: fatigue screening of implant cushioning polymers and shock-absorbing components under physiological loading rates
  • Aerospace: validation of elastomeric vibration isolators and energy-absorbing structures across the operational temperature envelope
  • Metallurgy and power generation: low-cycle fatigue evaluation of components experiencing constrained thermal-mechanical strain cycling

FAQ

What is the difference between strain-controlled and stress-controlled fatigue testing?

In strain-controlled testing, the machine commands a fixed cyclic deformation and records the resulting stress, whereas in stress-controlled testing the load is fixed and the deformation is measured. Strain control is preferred for components whose deflection is geometrically constrained and for low-cycle fatigue of metals, because it captures cyclic softening and relaxation behavior directly.

Why does the peak compressive stress decrease during the test?

The stress decrease reflects cumulative fatigue damage mechanisms such as viscoelastic stress relaxation, molecular or microstructural rearrangement (cyclic softening), internal crack initiation and growth, and heat build-up that reduces material stiffness. The softening ratio is therefore a key indicator of degradation rate.

What strain ratio and strain amplitudes are typically used?

For cushioning and mounting materials, fully compressive cycling with a strain ratio above zero is standard, with strain amplitudes commonly ranging from a few percent for stiff rubbers to several tens of percent for soft foams. Metallic strain-controlled tests may span total strain amplitudes from approximately 0.2 percent in the transition region to several percent in the low-cycle fatigue regime.

How is heat build-up managed during testing?

Excessive self-heating changes the material state and invalidates comparisons, so frequency is limited, specimen temperature is monitored continuously, and forced-air cooling can be applied. If the application environment involves high-frequency vibration, dedicated heat build-up procedures following ASTM D623 may be performed separately.

How many specimens are required for a valid strain-life curve?

A minimum of three to five replicate specimens per strain amplitude, covering at least four to six amplitude levels, is generally recommended so that the resulting fatigue data can be analyzed statistically and fitted to strain-life models such as the Coffin-Manson relationship for metals or fatigue crack growth-based models for elastomers.

Can the test be combined with environmental conditioning?

Yes. Environmental chambers allow cyclic compression fatigue testing at elevated temperatures, subambient temperatures, controlled humidity, or in the presence of aging media, which is essential for evaluating thermo-oxidative aging effects and for validating materials intended for harsh service environments.