Formability
Automotive product designers target small radii for springback control, sectional stiffness, packaging constraints, and design features. These small radii lead to new challenges as applications for AHSS grades continue to increase. One of these challenges is an increased sensitivity to crack formation in those designs with small die radius to material thickness (R/T) ratios. Cracks forming at small R/T in AHSS grades are known as shear fractures.
General forming limit curves or other press shop criteria cannot predict shear fractures, nor are they flagged when traditional approaches are used in forming simulation packages. However, these shear fractures do occur in die tryout. Shear fractures are another form of local formability failure associated with multiphase AHSS such as DP and TRIP.
Shear fractures on AHSS may exhibit similarities to edge fracture, specifically the absence of necking prior to failure. This is in contrast with global formability failures, which are characterized by significant thinning near the fracture. Shear fractures occur almost immediately (within 1 mm of displacement) after reaching maximum load, meaning there is essentially no post-uniform elongation. This is contrary to the tensile behavior where significant post-uniform ductility remains prior to fracture.K-9
Figures 1 and 2 highlight the appearance of a crack on the bend radius caused by shear fracture. No thinning is observed, which is consistent with failures limited by local formability concerns.

Figure 1: Shear fracture in DP780.F-5

Figure 2: Shear fracture in DP980.D-7
Figure 3 shows a typical shear fracture on a DP780 part viewed from different angles. The shear fracture occurred on the sharp radius on the left whereas the larger radius on the right experienced no failure. Depth of draw and draw bead configuration were the same on both sides of the draw panel. Restraining force was also similar on both sides of the blankholder. The significant variable was the die radius.

Figure 3: Different Views of a DP780 Part with Small R/T Leading to Shear Fracture at Bead Radius. An R/T = 1.67 led to shear fracture on the left side of the image, while the symmetric area on the right side had an R/T = 4.4, with no shear fracture even though it had the same depth of draw, draw bead configuration, and restraining force.U-6
It is helpful to describe the characteristic differences between conventional tensile fracture and shear fracture, as shown in Figure 4. A conventional tensile fracture is called a Type I fracture, and has been the typical fracture type historically encountered. Type I fractures occur off the radius, and is preceded by necking or metal thinning. Successful prediction of this type of fracture occurs with conventional application of strain analysis and Forming Limit Diagrams. This is in contrast with shear fracture – categorized as a Type III fracture – which occurs within the die radius, with no thinning from necking (typical for local formability failures). Type II fractures occur at or near the tangent of the radius in metal drawn over the radius.

Figure 4: Schematic descriptions of different fracture types ranging from shear fracture to conventional tensile fracture.S-19
Numerous studies show that radius to thickness ratios (R/T) are significant indicators of performance with respect to shear fracture on AHSS. This research led to the establishment of R/T ratio guidelines. While bend testing also categorizes products based on achievable R/T, the significant difference is that the ends are not restrained in a standard bend test. Shear fracture testing typically involves some type of restraining force, such as that seen in a Bending Under Tension test.
As with edge fracture, AHSS grades may be available at a similar strength but with improved minimum R/T ratio. Guidelines have been established for minimum R/T ratios based on bend test results as well as real world case studies. For DP340/590 and above, the R/T ratio should be at least 3T for product features such as embossments where there is relatively limited metal motion. Pulling these grades across a radius or through a draw bead under tension increases the minimum R/T ratio to at least 5T.
As strength levels increase, it is necessary to increase R/T ratios to avoid shear fractures. One study recommended a minimum R/T of 8 for DP800W-4 while another has a critical R/T of at least 7T for DP980S-19. Differences such as these are likely due to different test conditions such as the tension applied during bending, test speed and lubrication. Higher deformation rates (forming speed) and better lubrication tends to promote shear fracture and cause fracture on material close to the die radius.S-19 A combination of high forming speed and back tension leads to DP590 and DP780 having a critical R/T value of 12, with DP980 having a critical R/T of over 16.S-20
Shear fracture is sensitive to rolling direction. If the radius is running in the rolling direction, the bend will be transverse to the rolling direction which is the worst-case scenario when trying to avoid shear fracture. Understanding the directionality of minimum R/T ratios when designing the part to avoid shear fractures is therefore important. One study evaluated DP780, which discovered a critical minimum R/T of 5 to avoid shear fracture, although this varied with back tension and pulling speed. At all R/T ratios tested, the samples oriented so the bend radius was parallel to the rolling direction failed at lower stress than if the bend radius was perpendicular (transverse) to the rolling direction. Tighter R/T magnifies this effect, as does a higher strength grade. At 1.5 R/T, shear fracture with bends perpendicular to the rolling direction occurred when the stress reached 81% of the tensile strength, where in samples with the bend parallel to the rolling direction, failure occurred at 66% of the tensile strength.S-21
Microstructure also plays a role. Phase distribution uniformity, fine microstructural phases, and a decrease in hardness ratio between martensite and ferrite all increase formability as measured by the smallest achievable R/T resulting in split-free panels.W-4, H-6 These are the same factors that result in improved hole expansion values.
Forming Limit Curves are the limiting strain states based on the onset localized deformation, or necking. Generating conventional FLCs typically involves using a 100mm diameter hemispherical punch to deform 1mm to 2mm thick sheet steels, resulting in R/T ratios of 25 or higher. Many decades of use have shown that conventional FLC approaches can be used to assess part robustness and predict failure in areas having large R/T ratios and failure modes affected by global formability. These show up as Type I fractures.
When the R/T ratio is within the shear fracture limit but above the simple bending limit (no stretching imposed to bending), failure may occur in the radius or outside the radius, depending upon the tension level applied during forming. If the failure occurs inside the radius, the failure limit derived from the shear fracture tests should be used as the criterion to predict failure. Finally, when the R/T ratio is smaller than the limit from the simple bending test, the failure occurs in the radius.
In addition to large R/T, most Forming Limit Curves are generated from tests are conducted at a very low strain rate, maintaining an isothermal condition (no heat generated from deforming the sheets). While these conditions are consistent with those adopted for the simulations, they differ significantly from those encountered in industrial practice.
Ignoring the role of deformation-induced heating is one of the most significant reason for the limited success of shear fracture prediction in conventional forming simulation. Strain rates for stamping are typically 1,000x to 10,000x greater than the strain rates for tensile testing. Contact between the sheet metal and the tooling at tight radii also drives up the local temperature. Maximum temperature at the die-sheet interface of 70°C has been found on DP590, but 105°C for CP800.F-6 Stamping DP780 leads to die temperatures of 180°C and blank temperatures of 108°C.P-11 Stamping DP980 produces contact temperatures of over 200°C in certain conditions.F-28
Using a simulation model that accounts for the thermal effects of forming and the associated response in the sheet metal, along with the traditional mechanical deformation response, has been shown to dramatically improve simulation accuracy to predict when shear fracture will occur.K-9, S-20, S-22
Therefore, it is important for the part designer to design an appropriate die radius for a given AHSS product and forming conditions / processes used to manufacture the part. Forming simulation is an excellent tool to derive an appropriate die radius for the specified part and forming process, recognizing that the failure criterion in the simulation must incorporate all conditions and failure modes encountered, including shear fracture.
Key Points
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- AHSS grades are at risk of crack formation in designs with small die radius to material thickness (R/T) ratios. These cracks are known as shear fracture.
- The strains associated with shear fracture are below that which are associated with the Forming Limit Curve.
- As with edge fractures, shear fractures are also a function of microstructure, strength level, and rolling direction. Consider these variables when designing parts and conducting die try-outs with prototype steel.
Citations
Citation:
K-43. K. Kahoul and B. Caekaert, “ArcelorMittal Belgium produces 3rd Generation AHSS incl. Q&P on the unique annealing furnace from ANDRITZ Metals,” Presented at the 12th International Conference on Zinc & Zinc Alloy Coated Steel Sheet – GALVATECH 2021, June 2021.
2ndGen AHSS, AHSS, Steel Grades
TWinning Induced Plasticity (TWIP) steels have the highest strength-ductility combination of any steel used in automotive applications, with tensile strength typically exceeding 1000 MPa and elongation typically greater than 50%.
TWIP steels are alloyed with 12% to 30% manganese that causes the steel to be fully austenitic even at room temperature. Other common alloying additions include up to 3% silicon, up to 3% aluminum, and up to 1% carbon. Secondary alloying additions include chromium, copper, nitrogen, niobium, titanium, and/or vanadium.D-29 The high alloying levels and substantially greater levels of strength and ductility place these into the 2nd Generation of Advanced High Strength Steels. Furthermore, due to the density of the major alloying additions relative to iron, TWIP steels have a density which is about 5% lower than most other steels.
Calling this type of steel TWIP originates from the characteristic deformation mode known as twinning. Deformation twins produced during sheet forming leads to microstructural refinement and high values of the instantaneous hardening rate (n-value). The resultant twin boundaries act like grain boundaries and strengthen the steel. On either side of a twin boundary, atoms are located in mirror image positions as indicated in the schematic microstructure shown in Figure 1. Figure 2 highlights the microstructure of TWIP steel after annealing and after deformation.

Figure 1: Schematic of TWIP steel microstructure.

Figure 2: TWIP steel in the annealed condition (left) and after deformation (right) showing deformation twins. The number of deformation twins increases with increasing strain.K-42
EDDS or Interstitial-Free or Ultra-Low Carbon steels are different descriptions for the most formable lower-strength steel. Possible test results for this grade are 150 MPa yield strength, 300 MPa tensile strength, 22% to 25% uniform elongation, and 45% to 50% total elongation. In contrast, test results on TWIP steels may show 500 MPa yield strength, 1000 MPa tensile strength, 55% uniform elongation, and 60% total elongation.
The stress-strain curves for these two grades are compared in Figure 3. The TWIP curves show the manifestation of Dynamic Strain Aging (DSA), also known as the PLC effect, with more details to follow.

Figure 3: Uniaxial tensile stress-strain curves for an interstitial-free (IF) extra-deep-drawing steel and an austenitic Fe-18%Mn-0.6%C-1.5%Al TWIP steel. Curves are presented both terms of engineering (s,e) and true (σ,ε) stresses and strains, respectively.D-30
Figure 4 compares the results of bulge testing ferritic interstitial-free (IF) steel and austenitic Fe-18%Mn-0.6%C-1.5%Al TWIP steel. The TWIP steel is still undamaged at a dome height that is 31% larger than the IF steel dome height at failure.D-30

Figure 4: Comparison of dome testing between EDDS and TWIP.D-30
Excellent stretch formability is associated with high n-values. Shown in Figure 5 is a plot showing how the instantaneous n-value changes with applied strain. N-value increases to a value of 0.45 at an approximate true (logarithmic) strain of 0.2 and then remains relatively constant until an approximate true strain of 0.3 before increasing again. The high and uniform n-value delays necking and minimizes strain peaks. Twins continue to form at higher strains, leading to finer microstructural features and continued increases in n-value at higher strains.

Figure 5: Instantaneous n-value changes with applied strain. TWIP steels have high and uniform n-value leading to excellent stretch formability.C-30
A microstructural deformation phenomenon known as the Portevin-LeChatelier (PLC) effect occurs when deforming some TWIP steels to higher strain levels. The PLC effect is known by several other names as well, including jerky flow, discontinuous yielding, and dynamic strain aging (DSA).
The severity varies with alloy, strain rate, and deformation temperature. Figure 6 shows how DSA affects the appearance of the stress strain curve of two TWIP alloys.D-29 The primary difference in the alloy design is the curves on the right are for steel containing 1.5% aluminum, with the curves on the left for a steel without aluminum. The addition of aluminum delays the serrated flow until higher levels of strain. Note that both alloys have negative strain rate sensitivity.

Figure 6: Influence of aluminum additions on serrated flow in Fe-18%Mn-0.6%C TWIP (Al-free on the left) and Fe-18%Mn-0.6%C-1.5% Al TWIP (Al-added on the right).D-29
The primary macroscopic manifestations of the Portevin-LeChatelier (PLC) effect areD-29:
- negative strain rate sensitivity.
- stress-strain curve showing serrated or jerky flow, indicating non-uniform deformation. Strain localization takes place in propagating or static deformation bands.
- the strain rate within a localized band is typically one order of magnitude larger, while that outside the band is one order of magnitude lower, than the applied strain rate.
- limited post-uniform elongation, meaning uniform elongation is just below total elongation. Said another way, fracture occurs soon after necking initiation.
The PLC effect leads to relatively poor sheared edge expansion, as measured in a hole expansion test. Figure 7 on the left highlights the crack initiation site in a sample of highly formable EDDS-IF steel, showing the classic necking appearance with extensive thinning prior to fracture. In contrast, note the absence of necking in the TWIP steel shown in the right image in Figure 7.D-29

Figure 7: Sheared edge ductility comparison between IF (left) and TWIP (right) steel. TWIP steels lack the sheared edge expansion capability of IF steels.D-29
The stress-strain curves of several TWIP grades are compared in Figure 8.

Figure 8: Engineering stress-strain curve for several TWIP Grades.P-18
Complex-shaped parts requiring energy absorption capability are among the candidates for TWIP steel application, Figure 9.

Figure 9: Potential TWIP Steel Applications.N-24
Early automotive applications included the bumper beam of the 2011 Fiat Nuova Panda (Figure 10), resulting in a 28% weight savings and 22% cost savingsN-24 over the prior model which used a combination of PHS and DP steels.D-31

Figure 10: Transitioning to a TWIP Bumper Beam Resulted in Weight and Cost Savings in the 2011 Fiat Nuova Panda. N-24, D-31
In the 2014 Jeep Renegade BU/520, a welded blank combination of 1.3 mm and 1.8 mm TWIP 450/950 (Figure 11) replaced a two-piece aluminum component, aiding front end stability while reducing weight in a vehicle marketed for off-road applications.D-31

Figure 11: A TWIP welded blank improved performance and lowered weight in the 2014 Jeep Renegade BU/520.D-31
Also in 2014, the Renault EOLAB concept car where the A-Pillar Lower and the Sill Side Outer were stamped from TWIP 980 steel.R-21 By 2014, GM Daewoo used TWIP grades for A-Pillar Lowers and Front Side Members, and Hyundai used TWIP steel in 16 underbody parts. Ssangyong and Renault Samsung Motors used TWIP for Rear Side Members.I-20
Other applications include shock absorber housings, floor cross-members, wheel disks and rims, wheelhouses, and door impact beams.
A consortium called TWIP4EU with members from steel producers, steel users, research centers, and simulation companies had the goal of developing a simulation framework to accurately model the complex deformation and forming behavior of TWIP steels. The targeted part prototype component was a backrest side member of a front seat, Figure 12. Results were published in 2015.H-58

Figure 12: TWIP4EU Prototype Component formed from TWIP Steel.H-58
In addition to a complex thermomechanical mill processing requirements and high alloying costs, producing TWIP grades is more complex than conventional grades. Contributing to the challenges of TWIP production is that steelmaking practices need to be adjusted to account for the types and amounts of alloying. For example, the typical ferromanganese grade used in the production of other grades has phosphorus levels detrimental to TWIP properties. In addition, high levels of manganese and aluminum may lead to forming MnO and Al2O3 oxides on the surface after annealing, which could influence zinc coating adhesion in a hot dip galvanizing line.D-29
Forming Modes
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The usual mode of bending is curvature around a straight-line radius (Figure 1). Through the thickness is a gradient of strains from maximum outer fiber tension (the outermost surface) through a neutral axis to inner fiber compression (the surface closest to the punch or bend axis). No strain occurs along the bend axis in the direction parallel to the bend axis, and therefore is in plane strain. The discussion below considers only bulk deformation, and excludes the implications of any edge effects. Bend testing procedures are linked here.

Figure 1: Typical bend where the outer surface is in tension, and the inner surface is in compression. A neutral axis lies in between.S-23
When sheet metal flows through draw beads or over the die radius into the punch opening, it is bent, straightened, and in the case of draw beads re-bent in the opposite direction. The net strain after this process may be relatively small. However, each of the sequential bending and unbending steps strain hardens the sheet metal, which reduces the ability for further deformation of the metal in subsequent operations.
Deformation at the outer surface during three-point bending depends on the stretchability capacity of the metal. The failure strain in the bend is related to the total elongation of conventional steel, but AHSS grades with multiphase microstructures such as DP and TRIP experience shear fracture that severely reduces the bendability before failure occurs. A higher total elongation helps sustain a larger outer fiber stretch of the bend before surface fracture, thereby permitting a smaller bend radius. Since total elongation decreases with increasing strength for a given sheet thickness, the minimum design bend radius must be increased (Figure 2).

Figure 2: Larger bend radius is needed as the total elongation decreases.S-23
The ratio of punch radius to sheet thickness, or the r/t ratio, allows for calculation of the amount of elongation on the outermost surface. This value can be compared against the total elongation of the metal as determined in a tensile test, or against the minimum elongation value allowed in the specification. If the part geometry will not allow for sufficient elongation for the selected metal grade, then either the part, process, or steel grade must change. [Note that this is not a perfect assessment, since elongation in a tensile test is measured relative to a 50 or 80 mm gauge length, which is likely different than the dimensions of the bent section.]
For design and springback control, usually a smaller r/t ratio is desirable. However, this may not be suitable in terms of formability. Increased material strength usually is associated with a reduction in total elongation, which in turn means a successful bend requires a larger r/t ratio.
For equal strengths, most AHSS grades have higher total elongations than conventional HSLA steels. However, several AHSS grades have limited local formability based on their microstructure, and may be at risk for cracking during edge expansion.
Cracking in production stamping conditions at stress levels below what is predicted with Forming Limit Diagrams may be attributed to these local formability failures. As an illustration, physical bend tests and simulations were performed for both HSLA and DP780 steels.S-11 The HSLA global formability failure aligned with simulation predictions (Figure 3), and was accompanied by a visible neck (Figure 4). In contrast, the DP780 showed no visible neck at the failure site (Figure 5) and no correlation between the simulation and actual test results (Figure 6).
Like hole expansion, bending limits in AHSS products are further lowered by shear fracture associated with the interfaces between the ductile ferrite and the hard martensite phase in the microstructure. This reduction becomes more severe as the strength increases, since increasing strength is achieved by increasing the volume of the hard martensite phase. More about shear fracture is found here.

Figure 3: Forming simulation of HSLA with strong correlation to actual testing.S-11

Figure 4: Close-up of visible necking before tensile failure in HSLA.S-11

Figure 5: Comparison of forming simulation with actual testing of the DP780. Note lack of correlation.S-11

Figure 6: Close-up of local formability failure on DP780 with no visible necking before failure.S-11
Rotary Bending
One way to address springback involves the use of rotary benders. Rotary benders transfer the vertical movement of a press stroke into a precise, rotary forming motion. A rocker or rotating die can simultaneously hold, bend, and overbend the sheet past 90° to counter material springback (Figure 7).

Figure 7: The rotation of the rocker bends the sheet metal around the anvil with less pressure than needed for wipe toolsD-8
Use rotary bending tooling where possible instead of flange wipe dies. Rotary bending allows for easy adjustment of the bending angle to correct for changes in springback due to variations in steel properties, die set, lubrication, and other process parameters. In addition, the tensile loading generated by the wiping shoe is absent.
There are four sequential steps to the process:
1) Downward pressure from the rocker clamps the part with the bending lobes before bending starts
2) Induced rotation of the rocker bends material around the anvil
3) The rocker bends the sheet metal past final angle to compensate for springback
4) The rocker releases the sheet metal to allow springback to desired angle
Using rotary benders to roll darts into the part during bending provides another way to reduce springback and stiffen the part (Figure 8).

Figure 8: Stiffening darts can be created as part of the rotary bending operation.R-7
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Citations
Citation:
C-31. F.G. Caballero, S. Allain , J. Cornide , J.D. Puerta Velásquez , C. Garcia-Mateo and M.K. Miller, “Design of Cold Rolled and Continuous Annealed Carbide-Free Bainitic Steels for Automotive Application,” Materials & Design, Volume 49, August 2013, Pages 667-680, doi.org/10.1016/j.matdes.2013.02.046.