strain hardening exponent

{{Short description|Measurement in material science}}

{{Context|date=June 2021}}

The strain hardening exponent (also called the strain hardening index), usually denoted n, is a measured parameter that quantifies the ability of a material to become stronger due to strain hardening. Strain hardening (work hardening) is the process by which a material's load-bearing capacity increases during plastic (permanent) strain, or deformation. This characteristic is what sets ductile materials apart from brittle materials.{{Cite journal |last=Scales |first=M. |last2=Kornuta |first2=J.A. |last3=Switzner |first3=N. |last4=Veloo |first4=P. |date=2023-12-01 |title=Automated Calculation of Strain Hardening Parameters from Tensile Stress vs. Strain Data for Low Carbon Steel Exhibiting Yield Point Elongation |url=https://doi.org/10.1007/s40799-023-00626-4 |journal=Experimental Techniques |language=en |volume=47 |issue=6 |pages=1311–1322 |doi=10.1007/s40799-023-00626-4 |issn=1747-1567|url-access=subscription }} The uniaxial tension test is the primary experimental method used to directly measure a material's stress–strain behavior, providing valuable insights into its strain-hardening behavior.

The strain hardening exponent is sometimes regarded as a constant and occurs in forging and forming calculations as well as the formula known as the Hollomon equation (after John Herbert Hollomon Jr.) who originally posited it as:

\sigma=K\epsilon^nJ. H. Hollomon, Tensile deformation, Trans. AIME, vol. 162, (1945), pp. 268-290.

where \sigma represents the applied true stress on the material, \epsilon is the true strain, and K is the strength coefficient.

The value of the strain hardening exponent lies between 0 and 1, with a value of 0 implying a perfectly plastic solid and a value of 1 representing a perfectly elastic solid. Most metals have an n-value between 0.10 and 0.50. In one study, strain hardening exponent values extracted from tensile data from 58 steel pipes from natural gas pipelines were found to range from 0.08 to 0.25, with the lower end of the range dominated by high-strength low alloy steels and the upper end of the range mostly normalized steels.

Tabulation

class="wikitable"

|+ Tabulation of n- and K-values for several alloys {{Citation

| first = William D | last = Callister, Jr.

| title = Fundamentals of Materials Science and Engineering

| place = United States of America

| publisher = John Furkan & Sons

| edition = 2nd

| year = 2005

| page = 199

| isbn = 978-0-471-47014-4

}}{{Citation

| first = S | last = Kalpakjian

| title = Manufacturing engineering and technology

| place = Singapore

| publisher = Pearson Education South Asia Pte

| edition = 2nd

| year = 2014

| page = 62

}}{{Cite book|url=https://www.worldcat.org/oclc/21034891|title=ASM handbook|publisher=ASM International. Handbook Committee.|year=2005|isbn=978-0-87170-377-4|edition=10th|location=Materials Park, Ohio|pages=482|chapter=41.2 Roll Formed Aluminum Alloy Components|oclc=21034891}}

! Material !! n !! K (MPa)

Aluminum 1100–O (annealed)0.20180
2024 aluminum alloy (heat treated—T3)0.16690
5052-O

|0.13

|210

Aluminum 6061–O (annealed)0.20205
Aluminum 6061–T60.05410
Aluminum 7075–O (annealed)0.17400
Brass, Naval (annealed)0.49895
Brass 70–30 (annealed)0.49900
Brass 85–15 (cold-rolled)0.34580
Cobalt-base alloy (heat-treated)0.502,070
Copper (annealed)0.54325
AZ-31B magnesium alloy (annealed)0.16450
Low-carbon steel (annealed)0.26530
Low-carbon steel (cold worked)

|0.08

|700

4340 steel alloy (tempered @ 315 °C)0.15640
304 stainless steel (annealed)0.4501275

References

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