Application Note | Coating Adhesion Testing
Understanding Coating Failures Using Scratch Testing
Critical Loads, Failure Modes, and Detection Methods Across AlCrN, DLC, TiN, and CD Coatings

Research & Experimental Testing
Jocelyn Esparza & Pierre Leroux
Visual Design & Editorial
Andrew Shore
Introduction
Surface engineering of materials plays a significant role in a variety of functional applications, ranging from decorative appearance to protecting substrates from wear, corrosion and other forms of deterioration. Important factors that determine the quality and service lifetime of coatings are their cohesive and adhesive characteristics.
Why Understanding Coating Failures Matters
Heavens[1] developed the scratch test for adhesion evaluation for the first time in 1950. Benjamin and Weaver[2] proposed critical load, Lc, as a quantitative value to evaluate the coating adhesion. The scratch test has become one of the most widely applied methods to evaluate coating adhesion. Over the past two decades, this technique has been extensively used to assess the adhesion of PVD/CVD deposited super-hard nanocomposite coatings, which usually exhibits a high residual stress at the coating/substrate interface. Moreover, the scratch test is an essential tool for quality control of materials used in wear/abrasive environments, allowing us to detect premature adhesive/cohesive failure of coatings in real-life applications.
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Measurement Objectives
The process of scratching is carried out in a controlled and monitored manner to observe moments of adhesive and cohesive failures. In this study, different coatings were tested and compared using the NANOVEA PB1000 Mechanical Tester (see Fig. 1) to showcase the capacity of the instrument to investigate the adhesive and cohesive failure behaviors of different coatings during the scratch tests.
Measurement Principle

The scratch testing method is a very reproducible, quantitative technique. Critical loads at which failures appear are used to compare the cohesive or adhesive properties of coatings or bulk materials. During the test, scratches are made on the sample with a sphero-conical stylus (tip radius ranging from 1 to 200 µm) which travels at a constant speed across the sample, under a constant load, or a progressive load with a fixed loading rate.
When performing a progressive load test, the critical load is defined as the smallest load at which a recognizable failure occurs. In the case of a constant load test, the critical load corresponds to the load at which a regular occurrence of such failure along the track is observed.
In the case of bulk materials, the critical loads observed are cohesive failures, such as cracking or plastic deformation of the material. In the case of coated samples, the lower load regime often results in conformal or tensile cracking of the coating without full delamination. In the higher load regime, further damage usually comes from coating detachment from the substrate by spalling, buckling or chipping. Fig. 2 illustrates the principle of scratch testing.

Comments on the Critical Load
The scratch test gives very reproducible, quantitative data that can be used to compare the behavior of various coatings. The critical loads depend on the mechanical strength (adhesion, cohesion) of a coating-substrate composite, but also on several other parameters: some of them are directly related to the test itself, while others are related to the coating-substrate system. The parameters that influence the critical loads are summarized in Table 1.
| Test-specific parameters | Sample-specific parameters |
|---|---|
| Loading rate | Friction coefficient between surface and indenter |
| Scratching speed | Internal stresses in the material (bulk materials) |
| Indenter tip radius | Material hardness and roughness (coating-substrate systems) |
| Indenter material | Substrate hardness and roughness |
| Coating hardness and roughness | |
| Coating thickness |
Table 1: List of parameters that influence the critical loads.
The strength of scratch testing comes from the reproducibility of the test and the sensitivity to detect quantitatively small changes in the cohesive and adhesive properties that comes from changes in coating manufacturing processes or batch variations.
Means for Critical Load Determination
Test Procedure
The NANOVEA Mechanical Tester (micro module) equipped with a sphero-conical diamond stylus was used to perform progressive load scratch tests on a variety of different coated samples. The test parameters of each material are listed in Table 2, and the tip geometries are given in Fig. 3.
| Coating | Aluminum chromium nitride (AlCrN) | Diamond-like carbon (DLC) | Titanium nitride (TiN) | CD |
|---|---|---|---|---|
| Load type | Progressive | Progressive | Progressive | Progressive |
| Initial load | 0.2 N | 0.01 N | 0.5 N | 0.1 N |
| Final load | 8 N | 15 N | 125 N | 25 N |
| Loading rate | 8 N/min | 30 N/min | 75 N/min | 25 N/min |
| Scratch length | 3.0 mm | 3.0 mm | 4.5 mm | 20.0 mm |
| Scratch speed | 3.0 mm/min | 6.0 mm/min | 2.7 mm/min | 20 mm/min |
| Indenter geometry | 120° cone | 90° cone | 120° cone | 120° cone |
| Indenter tip material | Diamond | Diamond | Diamond | Diamond |
| Indenter tip radius | 50 µm | 20 µm | 200 µm | 200 µm |
Table 2: Test parameters.

Results and Discussion
AlCrN Coating
In the tooling industry, studying the adhesive and frictional properties of a coating that is applied to cutting tools supports R&D efforts of creating an optimal coating for every tooling application. One type of coating material known as aluminum chromium nitride (AlCrN) was measured for this study. After the scratch test was performed, cracking started to appear within the scratched region and the acoustic emissions showed a spike in energy when the coating first failed. This occurred at a critical load (Lc1) of 1.36 N which is marked in the Fig. 4 graph and Fig. 6 micrograph. The acoustic emissions appear to stabilize once the indenter applies a normal force of 2.71 N or more, which is the second critical load (Lc2). The scratch shows visual signs of complete delamination at this point as well. The coefficient of friction is constant until failure starts, with an increasing coefficient of friction. As the tip passes through the coating and reaches the substrate in this zone, the coefficient of friction varies but on average it is fairly stable until the tip penetrates deeper in the substrate toward the end of the scratch. True and residual depths are shown in Fig. 5. Full 3D profiles taken by white light chromatic technique are shown in Fig. 7. 2D profiles along the scratch and perpendicular to the scratch are shown in Fig. 8. This allows the study of pile up and the calculation of the volume displaced by the scratch test.





| Profile | Maximum depth (µm) | Maximum height (µm) |
|---|---|---|
| Profile along the scratch | 10.96 | 0.9699 |
| Profile across the scratch | 11.00 | 8.985 |
Table 3: Maximum depth and height of the AlCrN scratch profiles shown in Fig. 8.
Diamond-Like Carbon
The diamond-like carbon, DLC, film exhibits a scratch track with a peculiar serrated pattern above Lc1 of 3.5 N as shown in Fig. 9. Small periodic localized hemispherical coating chipping occurs at the side of the scratch track, indicating weak cohesive strength of this sample. Such a chipping phenomenon results in oscillations in the Friction Force as presented in Fig. 10. A complete removal of DLC coating in the scratch track takes place at Lc2 of 7.5 N.


TiN Coating
The titanium nitride (TiN) coating showed signs of cracking based on the acoustic emissions data represented in Fig. 11 at a critical load (Lc1) of 51.1 N. Visual signs of cracking did not occur at this location but acoustic emissions allow the user to detect cracking when it is not easily visible under microscope inspection. The second critical load (Lc2) location occurs at 79.1 N, visible signs of complete delamination occur on the scratch in Fig. 12 as well as increased spikes in the acoustic emissions after this point.


CD Coating
Scratch resistance is an important factor determining the service lifetime of CD/DVD. The CD is composed of a 1.2 mm disc of polycarbonate with a thin layer of aluminum. The aluminum is protected by a film of lacquer as illustrated in Fig. 13. Fig. 14 shows the evolution of coating behavior during the scratch test. The initial mark on the label layer appears at the beginning of the test (a). As the stylus continues to penetrate into the coating, failure of the label (top) layer takes place at 3.2 N (b). Between 3 and 6 N, the label continues to delaminate while the aluminum layer remains adherent (c), until a load of 6.2 N is reached where large spallation of the aluminum layer takes place (d). Such a coating evolution can also be indicated by the progressive increase of friction coefficient as shown in Fig. 15.



Summary of Critical Loads
| Coating | Lc1 (N) | Lc2 (N) | Failure observed |
|---|---|---|---|
| AlCrN | 1.36 | 2.71 | Cracking with an acoustic emission spike; complete delamination at Lc2 |
| DLC | 3.5 | 7.5 | Periodic hemispherical chipping beside the track; complete removal at Lc2 |
| TiN | 51.1 | 79.1 | Cracking detected by acoustic emission before it is visible; delamination at Lc2 |
| CD | 3.2 | 6.2 | Label (top) layer failure; large spallation of the aluminum layer |
Table 4: Critical loads of the four coatings, as reported above.
Conclusion
The NANOVEA Mechanical Tester is a superior tool for scratch and marring quality control of a variety of coatings. Different coatings exhibit drastically different adhesion/cohesion failures as demonstrated in the scratch tests. By applying loads in a controlled and closely monitored fashion, the tool allows users to identify quantitative and reproducible critical load failures. This type of information can help manufacturers improve and control the quality of their coatings.
The Nano and Micro modules of the NANOVEA Mechanical Tester all include ISO and ASTM compliant indentation, scratch and wear tester modes, providing the widest and most user friendly range of testing available in a single system. NANOVEA’s unmatched range is an ideal solution for determining the full range of mechanical properties of thin or thick, soft or hard coatings, films and substrates, including hardness, adhesion, wear resistance and many others.
In addition, optional 3D non-contact profiler and AFM module are available for high resolution 3D imaging of indentation, scratch and wear track in addition to other surface measurements such as roughness.
References
1. Heavens, O.S., Some factors influencing the adhesion of films produced by vacuum evaporation. J. Phys. Radium, 1950. 11: p. 355–360.
2. Benjamin, P. and C. Weaver, Measurement of Adhesion of Thin Films. Proceedings of the Royal Society, 1960. 254: p. 163–176.
3. Bull, S.J., Failure mode maps in the thin film scratch adhesion test. Tribology International, 1997. 30(7): p. 491–498.
Frequently Asked Questions About Coating Failures in Scratch Testing
What is a critical load in scratch testing?
In a progressive load test, the critical load is the smallest load at which a recognizable failure occurs. In a constant load test, it is the load at which such a failure occurs regularly along the track. Critical loads compare the cohesive or adhesive properties of coatings and bulk materials.
What is the difference between cohesive and adhesive coating failure?
Cohesive failure happens within the coating, such as conformal or tensile cracking and chipping, usually in the lower load regime. Adhesive failure happens at the coating-substrate interface, with detachment by spalling, buckling or chipping and eventually delamination, usually at higher loads.
How are coating failures detected during a scratch test?
By microscopic observation of the track, tangential (frictional) force recording, acoustic emission detection of microcracks, and depth sensing of sudden changes or true and residual depth. 3D non-contact imaging and AFM can image the full scratch profile afterwards.
Which parameters influence the critical load?
Test parameters (loading rate, scratching speed, indenter tip radius and material) and sample parameters (friction between surface and indenter, internal stresses, substrate and coating hardness and roughness, and coating thickness).
What critical loads did the four coatings show?
AlCrN failed at Lc1 1.36 N and Lc2 2.71 N, DLC at 3.5 and 7.5 N, TiN at 51.1 and 79.1 N, and the CD label and aluminum layers at 3.2 and 6.2 N.
Can acoustic emission detect failures that are not visible?
Yes. On the TiN coating, acoustic emission signalled cracking at 51.1 N where no cracking was visible under the microscope, because AE detects the elastic waves of microcracks forming inside the coating.



