Residual Stress Measurement Techniques: XRD and Hole-Drilling
Residual stress measurement is essential wherever locked-in stress from welding, machining, heat treatment, or surface engineering influences fatigue life, distortion, or cracking risk. This guide develops the two most widely used practical measurement techniques, XRD sin-squared-psi and ASTM E837 hole-drilling, in depth, and positions them against neutron diffraction, contour, slitting, and magnetic methods for selecting the right technique for a given application.
Key Takeaways
- Residual stress is locked-in stress present with no external load applied, generated by non-uniform plastic deformation, thermal gradients, or phase transformation during manufacturing.
- XRD sin-squared-psi measurement is fully non-destructive but shallow, typically sampling only a few to a few tens of microns, making it well suited to fine spatial mapping of near-surface stress.
- ASTM E837 hole-drilling uses a strain gauge rosette and a small incrementally drilled hole to profile residual stress to roughly 1 mm depth, and is classified as semi-destructive because it leaves a small hole in the component.
- ASTM E837 permits reliable results up to about 80% of yield strength for blind-hole drilling but only about 50% of yield strength for through-hole drilling, due to differing local stress concentration around each hole geometry.
- Neither XRD nor hole-drilling alone reaches the several-millimetre to full-thickness depths accessible by neutron diffraction or the fully destructive contour and slitting methods.
- Weld residual stress assessment programmes frequently combine XRD for fine near-surface mapping with hole-drilling for shallow subsurface depth profiling, since the two methods sample different depths and offer different spatial resolution.
What Is Residual Stress and Why Measure It?
Residual stress is stress that remains locked within a component after all external loads have been removed, generated by non-uniform plastic deformation, thermal gradients, or phase transformation during manufacturing processes such as welding, machining, casting, rolling, or heat treatment. Because residual stress superimposes directly on applied service stress, tensile residual stress can significantly reduce fatigue life and promote cracking, as discussed in our spalling failure and reheat cracking guides, while compressive residual stress, deliberately introduced by shot peening or similar treatments, can substantially improve fatigue performance. Quantifying residual stress is therefore essential for both root-cause failure analysis and for validating manufacturing processes intended to control it.
XRD Residual Stress Measurement: The Sin-Squared-Psi Method
X-ray diffraction residual stress measurement relies on the fact that elastic lattice strain, caused by residual or applied stress, produces a measurable shift in diffraction peak position relative to the strain-free interplanar spacing. The sin-squared-psi (sin²ψ) method measures this shift for a chosen lattice plane across a series of sample tilt angles, psi, relative to the diffraction plane normal, a technique developed in more depth in our dedicated XRD for metallurgical analysis guide.
Sin-squared-psi method (biaxial stress state, isotropic material): sigma_phi = (E / (1+nu)) * (1/d0) * (d(d)/d(sin^2 psi)) where: d0 = strain-free interplanar spacing E, nu = X-ray elastic constants sigma_phi = residual stress at the surface in direction phi
Because the technique relies on a diffracted beam that travels into and back out of the material, it samples only a shallow near-surface volume, typically a few to a few tens of microns depending on the X-ray source and material absorption. This shallow, non-destructive sampling makes XRD particularly well suited to fine-resolution mapping of near-surface stress variation, for example across a weld toe, a shot-peened surface, or a ground component, without physically altering the part.
Hole-Drilling Residual Stress Measurement: ASTM E837
Principle and Procedure
ASTM E837 specifies a well-established, general-purpose method for determining near-surface residual stress in isotropic, linearly elastic material. A specialized three-element strain gauge rosette is bonded to the component surface, and a small hole, commonly with a nominal diameter around 2 mm, is drilled at the rosette’s geometric centre using a high-speed air turbine or orbital milling technique specifically to minimize additional machining-induced stress. Removing stressed material from the hole location allows the surrounding material to relax, and this relaxation produces small but measurable strain changes at each of the three gauges, oriented at different angles around the hole to fully resolve the in-plane stress state.
Calculation Method
The relieved strains measured at each gauge are converted into the original residual stress using calibration coefficients, denoted a and b, that are tabulated in ASTM E837 for standard rosette geometries (Types A, B, and C) and were derived from finite element calculations. For a uniform stress field through the hole depth, the calculation reduces to a closed-form relationship between the three measured strains and the principal in-plane stresses and their orientation; for stress fields that vary with depth, the standard’s incremental method processes the strain readings collected at each successive drilling step to reconstruct a depth-resolved stress profile.
Uniform-stress hole-drilling relation (conceptual form):
e_j = (1/E) * [ a_jk * (sigma_x + sigma_y)/2
+ b_jk * (sigma_x - sigma_y)/2 * cos(2*theta)
+ b_jk * tau_xy * sin(2*theta) ]
where:
e_j = relieved strain measured at gauge j
a_jk, b_jk = tabulated calibration coefficients (ASTM E837)
sigma_x, sigma_y, tau_xy = in-plane residual stress components
theta = gauge angular position around the rosette
Blind-Hole vs. Through-Hole Drilling
| Parameter | Blind-Hole Drilling | Through-Hole Drilling |
|---|---|---|
| Applicable workpiece | Thick sections (hole stops before full penetration) | Thin sheet (hole penetrates full thickness) |
| Stress information | Depth-resolved profile via incremental drilling | Single depth-averaged (membrane) stress value |
| Reliable stress limit | Up to approximately 80% of yield strength | Up to approximately 50% of yield strength |
| Typical measurement depth | On the order of 1 mm | Full workpiece thickness |
Blind-hole drilling is the more commonly applied approach in practice, since incremental depth stepping allows a subsurface stress profile, valuable for characterizing shot-peened, case-hardened, or machined surface layers where stress varies significantly with depth, a topic connected to the hardening mechanisms covered in our quenching and tempering guide.
A Semi-Destructive, Not Non-Destructive, Method
Hole-drilling is classified as semi-destructive or minimally invasive because it leaves a small (commonly 1.5-2 mm diameter) hole in the component surface, in contrast to fully non-destructive XRD measurement. In many applications the resulting hole falls within the component’s acceptable design margin or can be filled and inspected afterward, but this distinction matters for highly critical or in-service components where any material removal requires engineering justification.
XRD vs. Hole-Drilling: Choosing the Right Method
| Characteristic | XRD (sin²ψ) | Hole-Drilling (ASTM E837) |
|---|---|---|
| Invasiveness | Fully non-destructive | Semi-destructive (small drilled hole) |
| Sampled depth | Few to few-tens of microns | Up to approximately 1 mm (incremental) |
| Lateral spatial resolution | Sub-millimetre, fine mapping possible | Set by rosette diameter, typically several mm |
| Equipment portability | Portable units available for field use | Portable, widely used in field and lab |
| Best suited to | Fine near-surface mapping, shot-peening/grinding QC | Subsurface depth profiling beneath surface treatment layers |
Neither method is universally superior; the choice depends on the depth and spatial resolution the application requires. Many weld residual stress assessment programmes, including those relevant to the restrained joint behaviour discussed elsewhere on this site, apply both techniques together: XRD to finely map near-surface stress variation across the weld toe and adjacent HAZ, and hole-drilling to establish the shallow subsurface depth profile beneath any surface treatment or decarburized layer.
Other Residual Stress Measurement Techniques
XRD and hole-drilling are the two most widely used practical techniques, but several others fill specific niches where deeper penetration, full destructive validation, or particularly rapid screening is required.
| Technique | Destructive? | Typical Depth Reach | Notes |
|---|---|---|---|
| Neutron diffraction | No | Several centimetres (true bulk) | Same principle as XRD but with penetrating neutrons; requires a reactor or spallation source facility |
| Contour method | Yes (fully destructive) | Full cross-section | Sections the part and measures resulting surface deformation to back-calculate the 2D stress map |
| Slitting (crack compliance) method | Yes (fully destructive) | Full cross-section (through-thickness profile) | Measures strain relief as an incremental slit is cut, similar in concept to hole-drilling but 1D through-thickness |
| Magnetic Barkhausen noise | No | Near-surface (material dependent) | Rapid screening for ferromagnetic materials only; correlates magnetic domain behaviour with stress |
When Deeper or Destructive Methods Are Justified
Neutron diffraction and the destructive contour and slitting methods are generally reserved for cases where XRD and hole-drilling cannot reach the depth of interest, such as characterizing bulk residual stress deep within a thick weld or a heavily worked forging, or where an independent, high-confidence validation of a less destructive method’s results is required for a critical component qualification programme.
Industrial Significance
Accurate residual stress measurement underpins fatigue life prediction, distortion control, and the qualification of stress-relief and surface treatment processes across welding, machining, and heat treatment operations. XRD and hole-drilling remain the two most widely deployed techniques precisely because they balance practical accessibility, reasonable cost, and adequate accuracy for the vast majority of near-surface residual stress questions encountered in fabrication quality control and failure investigation, reserving neutron diffraction and destructive methods for the smaller set of cases that genuinely require bulk or full-depth characterization.
Frequently Asked Questions
What is residual stress and why is it measured?
How does the XRD sin-squared-psi method measure residual stress?
How does the ASTM E837 hole-drilling method work?
What is the difference between blind-hole and through-hole drilling?
How deep into a component can hole-drilling and XRD measure residual stress?
Which method is better for measuring weld residual stress: XRD or hole-drilling?
Is hole-drilling a destructive test method?
What other residual stress measurement techniques exist besides XRD and hole-drilling?
Recommended Reference Reading
Residual Stress Measurement by X-Ray Diffraction (SAE)
Applied reference for the sin-squared-psi method and X-ray elastic constants.
View on AmazonHandbook of Residual Stress and Deformation of Steel
Comprehensive coverage of residual stress origins and measurement across steel processing.
View on AmazonASM Handbook Vol. 10: Materials Characterization
Reference coverage of residual stress measurement techniques alongside other characterization methods.
View on AmazonPractical Residual Stress Measurement Methods (Schajer, ed.)
Applied, technique-by-technique guide including hole-drilling, contour, and slitting methods.
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