Hubbry Logo
Charpy impact testCharpy impact testMain
Open search
Charpy impact test
Community hub
Charpy impact test
logo
8 pages, 0 posts
0 subscribers
Be the first to start a discussion here.
Be the first to start a discussion here.
Charpy impact test
Charpy impact test
from Wikipedia
A modern impact test machine.

In materials science, the Charpy impact test, also known as the Charpy V-notch test, is a standardized high strain rate test which determines the amount of energy absorbed by a material during fracture. Absorbed energy is a measure of the material's notch toughness. It is widely used in industry, since it is easy to prepare and conduct and results can be obtained quickly and cheaply. A disadvantage is that some results are only comparative.[1] The test was pivotal in understanding the fracture problems of ships during World War II.[2][3]

The test was developed around 1900 by S. B. Russell (1898, American) and Georges Charpy (1901, French).[4] The test became known as the Charpy test in the early 1900s due to the technical contributions and standardization efforts by Charpy.

History

[edit]

In 1896, S. B. Russell introduced the idea of residual fracture energy and devised a pendulum fracture test. Russell's initial tests measured un-notched samples. In 1897, Frémont introduced a test to measure the same phenomenon using a spring-loaded machine. In 1901, Georges Charpy proposed a standardized method improving Russell's by introducing a redesigned pendulum and notched sample, giving precise specifications.[5]

Definition

[edit]
A vintage impact test machine. Yellow cage on the left is meant to prevent accidents during pendulum swing, pendulum is seen at rest at the bottom

The apparatus consists of a pendulum of known mass and length that is dropped from a known height to impact a notched specimen of material. The energy transferred to the material can be inferred by comparing the difference in the height of the hammer before and after the fracture (energy absorbed by the fracture event).

The notch in the sample affects the results of the impact test,[6] thus it is necessary for the notch to be of regular dimensions and geometry. The size of the sample can also affect results, since the dimensions determine whether or not the material is in plane strain. This difference can greatly affect the conclusions made.[7]

The Standard methods for Notched Bar Impact Testing of Metallic Materials can be found in ASTM E23,[8] ISO 148-1[9] or EN 10045-1 (retired and replaced with ISO 148-1),[10] where all the aspects of the test and equipment used are described in detail.

Quantitative results

[edit]

The quantitative result of the impact tests the energy needed to fracture a material and can be used to measure the toughness of the material. There is a connection to the yield strength but it cannot be expressed by a standard formula. Also, the strain rate may be studied and analyzed for its effect on fracture.

The ductile-brittle transition temperature (DBTT) may be derived from the temperature where the energy needed to fracture the material drastically changes. However, in practice there is no sharp transition and it is difficult to obtain a precise transition temperature (it is really a transition region). An exact DBTT may be empirically derived in many ways: a specific absorbed energy, change in aspect of fracture (such as 50% of the area is cleavage), etc.[1]

Qualitative results

[edit]

The qualitative results of the impact test can be used to determine the ductility of a material.[11] If the material breaks on a flat plane, the fracture was brittle, and if the material breaks with jagged edges or shear lips, then the fracture was ductile. Usually, a material does not break in just one way or the other and thus comparing the jagged to flat surface areas of the fracture will give an estimate of the percentage of ductile and brittle fracture.[1]

Sample sizes

[edit]
Sample sizes[which?]

According to ASTM A370,[12] the standard specimen size for Charpy impact testing is 10 mm × 10 mm × 55 mm. Subsize specimen sizes are: 10 mm × 7.5 mm × 55 mm, 10 mm × 6.7 mm × 55 mm, 10 mm × 5 mm × 55 mm, 10 mm × 3.3 mm × 55 mm, 10 mm × 2.5 mm × 55 mm. Details of specimens as per ASTM A370 (Standard Test Method and Definitions for Mechanical Testing of Steel Products).

According to EN 10045-1 (retired and replaced with ISO 148),[10] standard specimen sizes are 10 mm × 10 mm × 55 mm. Subsize specimens are: 10 mm × 7.5 mm × 55 mm and 10 mm × 5 mm × 55 mm.

According to ISO 148,[9] standard specimen sizes are 10 mm × 10 mm × 55 mm. Subsize specimens are: 10 mm × 7.5 mm × 55 mm, 10 mm × 5 mm × 55 mm and 10 mm × 2.5 mm × 55 mm.

According to MPIF Standard 40,[13] the standard unnotched specimen size is 10 mm (±0.125 mm) x 10 mm (±0.125 mm) x 55 mm (±2.5 mm).

Impact test results on low- and high-strength materials

[edit]

The impact energy of low-strength metals that do not show a change of fracture mode with temperature, is usually high and insensitive to temperature. For these reasons, impact tests are not widely used for assessing the fracture-resistance of low-strength materials whose fracture modes remain unchanged with temperature. Impact tests typically show a ductile-brittle transition for high-strength materials that do exhibit change in fracture mode with temperature such as body-centered cubic (BCC) transition metals. Impact tests on natural materials (can be considered as low-strength), such as wood, are used to study the material toughness and are subjected to a number of issues that include the interaction between the pendulum and a specimen as well as higher modes of vibration and multiple contacts between pendulum tup and the specimen.[14][15][16]

Generally, high-strength materials have low impact energies which attest to the fact that fractures easily initiate and propagate in high-strength materials. The impact energies of high-strength materials other than steels or BCC transition metals are usually insensitive to temperature. High-strength BCC steels display a wider variation of impact energy than high-strength metal that do not have a BCC structure because steels undergo microscopic ductile-brittle transition. Regardless, the maximum impact energy of high-strength steels is still low due to their brittleness.[17]

See also

[edit]

Notes

[edit]
[edit]
Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
The Charpy impact test is a standardized high strain-rate method used to evaluate the of materials, particularly metals, by measuring the absorbed when a notched specimen is struck and fractured by a swinging . This test assesses a material's resistance to brittle under conditions, providing critical data on its ability to withstand sudden impacts without . Invented in 1900 by French materials scientist Georges Augustin Albert Charpy, the test was developed to address the need for quantifying material behavior at high loading rates, building on earlier pendulum-based impact concepts. Charpy's work, published in 1901, established the procedure using a simple-beam configuration with a V-notched specimen, which became a cornerstone for materials testing amid growing industrial demands for safer structures in the early . The test's relevance for evaluating brittle failure was demonstrated in analyses of tragedies like the Titanic disaster in 1912, which highlighted the dangers of brittle materials in cold environments. In the standard procedure, a rectangular bar specimen—typically 55 mm long, 10 mm wide, and 10 mm thick with a 2 mm deep V-notch—is supported horizontally at both ends and impacted at its midpoint by a released from a fixed height. The absorbed , expressed in joules, is determined from the pendulum's reduced swing height post-fracture, with results often averaged from multiple specimens tested at specified temperatures to map the ductile-to-brittle transition. Variations include subsize specimens for limited material availability or instrumented setups to capture force-time data for detailed analysis. The test is governed by international standards such as ASTM E23 for metallic materials and ISO 148, ensuring across laboratories worldwide. It is essential in industries including production, where it verifies weld and base metal performance; for component certification; and nuclear energy to monitor radiation-induced embrittlement in reactor vessels. Beyond metals, adaptations exist for polymers (ASTM D6110) and composites, though interpretations differ due to varying deformation mechanisms. Despite its simplicity, the Charpy test remains a vital tool for predicting real-world failure modes, with ongoing NIST verification programs maintaining accuracy in machine calibration and specimen preparation.

Introduction

Definition and Purpose

The Charpy impact test is a standardized pendulum-based method that evaluates the of materials by measuring the absorbed by a notched specimen when it is struck by a swinging hammer, leading to fracture. Developed and named after French scientist Georges Charpy, the test focuses on the material's ability to withstand sudden dynamic loads. The notched design of the specimen intentionally creates a point, simulating real-world defects or cracks that could initiate failure under impact. The primary purpose of the Charpy impact test is to quantify impact toughness, which reveals whether a exhibits ductile or brittle during rapid loading. This is critical for materials such as metals, polymers, and composites, where high absorbed energy indicates greater and resistance to , while low energy suggests . In engineering applications, the test supports by verifying material consistency, informs for load-bearing components, and enhances assessments by predicting failure risks in structures exposed to sudden impacts, such as in automotive or designs. A key application involves determining the ductile-to-brittle transition temperature, the point at which a material's mode shifts from energy-absorbing ductile tearing to low-energy brittle cleavage, particularly relevant for body-centered cubic metals like steels. Unlike static tensile tests that measure properties under slow, controlled loading, the Charpy test captures dynamic high-strain-rate responses essential for understanding real-time impact scenarios.

Basic Principle

The basic principle of the Charpy impact test involves the conversion of the pendulum's gravitational into upon release, which is then transferred to the notched specimen during impact, resulting in . The , typically released from a fixed , swings freely until it strikes the specimen positioned horizontally at the base. The absorbed by the specimen is determined by the difference in the pendulum's before impact and its residual after fracturing the specimen and completing its swing. This absorbed quantifies the material's resistance to sudden loading, primarily under high strain rates that simulate dynamic conditions. The absorbed energy EE is calculated using the formula E=mgh(cosθ2cosθ1)E = m g h (\cos \theta_2 - \cos \theta_1), where mm is the mass of the pendulum hammer, gg is the acceleration due to gravity, hh is the effective height from the pivot to the center of percussion (often equivalent to the pendulum arm length adjusted for the center of mass), θ1\theta_1 is the initial release angle, and θ2\theta_2 is the final angle after impact. This equation derives from the change in gravitational potential energy: the initial potential energy is mgh(1cosθ1)m g h (1 - \cos \theta_1), assuming the lowest point is the reference (zero potential), and the post-impact potential energy is mgh(1cosθ2)m g h (1 - \cos \theta_2). Subtracting these yields the absorbed energy in joules, with corrections applied for frictional losses in the machine bearings and air resistance to ensure accuracy. The derivation assumes negligible energy loss prior to impact and focuses on the height difference corresponding to the angular positions. In terms of , the V-notch in the specimen plays a critical role by creating a that induces a triaxial stress state at the notch root, promoting plane strain conditions due to the specimen's thickness and constraint. This triaxiality constrains flow, making the test sensitive to brittle mechanisms, particularly at low temperatures where cleavage dominates, characterized by transgranular separation along crystallographic planes with minimal deformation. At higher temperatures, ductile tearing prevails, involving void nucleation, growth, and coalescence with significant deformation, leading to a fibrous surface. The notch simulates real-world flaws like cracks or defects, amplifying local stresses to evaluate the material's toughness under constrained conditions. The total absorbed energy in the Charpy test comprises several components: elastic deformation stored and released before crack initiation, plastic deformation dissipated through yielding and necking around the notch, and fracture associated with crack initiation and propagation. is minor compared to plastic contributions in ductile materials, while in brittle regimes, fracture dominates with limited plasticity. These components collectively reflect the material's ability to redistribute stresses and delay unstable crack growth under impact.

Historical Development

Origins and Invention

The Charpy impact test emerged from late 19th-century efforts to evaluate material toughness under conditions, building on rudimentary drop-weight tests that had been used since the to assess performance in applications like weaponry and structural components. These early methods, such as those refined by S.B. Russell in 1898, involved dropping weights onto specimens to measure fracture energy, addressing growing concerns over brittle failures in industrial materials amid rapid production for railroads, bridges, and machinery. Although pendulum-based approaches existed in limited forms prior to 1900, they lacked standardization for notched specimens, limiting their ability to simulate real-world impact scenarios reliably. In 1901, French metallurgist Georges Augustin Albert Charpy, working at the École des Mines in , developed the impact test that bears his name, introducing a standardized apparatus to quantify the absorbed by a notched metal bar during fracture. This innovation was motivated by increasing reports of brittle fractures in pressure vessels, boilers, and ship hulls, where static tensile tests failed to predict behavior under sudden loads or low temperatures, prompting a need for dynamic assessment in the burgeoning industrial era. Charpy's design improved upon predecessors by using a swinging to strike a horizontally supported, V-notched specimen, providing repeatable measurements of absorbed in joules. Charpy detailed his apparatus and initial tests on various steels in a seminal 1901 paper published in the Annales des Mines, where he demonstrated the test's sensitivity to material composition, , and notch geometry, establishing it as a practical tool for . These early experiments revealed significant variations in fracture energy, highlighting the test's value in identifying brittle tendencies that could lead to catastrophic failures, a concern exemplified later by the 1912 Titanic disaster, which intensified focus on impact-resistant hull steels despite predating widespread adoption. This foundational work laid the groundwork for subsequent refinements, though standardization efforts would not gain traction until the post-World War I period.

Standardization and Evolution

Following its by Georges Charpy in 1901, the impact gained early formal recognition in , with references to standardized procedures appearing in technical by 1905. International efforts toward uniformity began in the early through organizations like the Association Internationale pour l'Essai des Matériaux, though full global standardization awaited later developments. The first major national standard emerged in the United States with ASTM E23-33T, published in 1933 as a tentative method for notched bar impact testing of metallic materials, establishing specifications for the Charpy pendulum apparatus, specimen geometry, and energy measurement. This standard was influenced by growing industrial needs for reliable toughness assessment and has undergone numerous revisions to address precision and applicability; revisions have included detailed guidelines for subsize specimens to accommodate thinner materials, with ongoing updates to further enhance accuracy. During World War II, the test's importance surged due to brittle fracture failures in ships and structures, prompting its widespread adoption for evaluating armor and structural steels to ensure ductility under impact. Post-war evolution saw the test integrated into regulatory frameworks, including ASME Boiler and Pressure Vessel Code sections for nuclear components, where Charpy results inform requirements for reactor vessels and piping. In the , advancements shifted from manual pendulums to automated and instrumented systems, enabling acquisition on , displacement, and initiation through computer-aided evaluation. Similar incorporation occurred in aerospace standards, such as those under SAE and FAA guidelines, for assessing material performance in high-stress environments. Prior to full harmonization, regional differences persisted; the EN 10045 (first published in 1990) specified Charpy V-notch testing with slight variations in verification procedures and temperature controls compared to ASTM E23. These were largely resolved through ISO 148, with the core standard ISO 148-1 first issued in 1983 and revised to its third edition in 2016, providing a unified method for impact testing of metallic materials. The 2016 version, confirmed current as of 2023 and still applicable in 2025, accommodates both V- and U-notch specimens while emphasizing machine calibration; meanwhile, the related ISO 14556:2023 update specifically addresses instrumented testing with digital instrumentation for enhanced load-time analysis.

Test Apparatus and Procedure

Equipment Components

The Charpy impact test apparatus consists of a robust pendulum-based designed to deliver a precise, high-velocity strike to a notched specimen while minimizing energy losses. The primary components include the pendulum , supporting frame, anvils and , measurement instruments, and safety features, all constructed to meet stringent standards for accuracy and reliability. The hammer, the core striking element, features a weighted arm typically capable of delivering initial energies ranging from 20 J to 300 J for standard metallic testing, though higher capacities up to 750 J are available for specialized applications. The hammer incorporates a striker tip, often made of durable for resistance to wear, with a standard radius of 2 (or 8 for certain configurations) to ensure consistent contact with the specimen. The is mounted on low-friction bearings to allow free swinging from an elevated release , usually around 140–150 degrees, achieving an impact of approximately 5 m/s. The machine frame provides a rigid, stable base to support the pendulum's oscillation and align the specimen horizontally, with the axis of rotation maintained parallel to a reference plane within tolerances of 2/1,000 to prevent misalignment-induced errors. Fixed anvils, spaced 40 mm apart (with a maximum deviation of 0.20 mm per ISO 148-2), form the supports beneath the specimen, ensuring the notch is centered and symmetrical within 0.5 mm of the mid-plane. A vise or clamp, either manual or pneumatic, secures the specimen ends against the anvils without introducing additional stress, using adjustable jaws to accommodate standard dimensions while avoiding deformation. Energy absorption is quantified using measurement tools such as a dial gauge, optical encoder, or digital display that records the difference in pendulum height before and after impact, calibrated to joules with a resolution of 0.5–1 J depending on capacity. Safety enclosures, typically transparent shields or interlocked guards, surround the area to contain flying fragments and protect operators from high-speed debris. Calibration verifies the machine's integrity per ISO 148-2, including direct checks for dimensional accuracy (e.g., striker alignment via imprint and anvil spacing) and dynamic tests for losses, which must not exceed 0.5–1% of nominal to ensure absorbed readings are within ±2 J or 1% accuracy. , air resistance, and bearing play (limited to ≤0.25 mm) are quantified using pendulums or instrumented strikers, with periodic indirect verification via certified specimens.

Step-by-Step Testing Process

The Charpy impact test procedure begins with preparation of the test specimen, which must be conditioned to the specified test temperature to simulate real-world service conditions. For standard room-temperature testing, the specimen is used as prepared, but for low-temperature evaluations, it is immersed in a controlled environment such as a liquid bath or cooling chamber; for cryogenic testing at -196°C, is used to cool the specimen for a minimum of 5 to 10 minutes to achieve uniform temperature throughout, ensuring the temperature is maintained within ±1°C during transfer to the test apparatus. The conditioned specimen is then quickly transferred to the testing position using insulated to minimize thermal recovery, typically within 5 seconds. In the setup phase, the notched specimen is securely positioned horizontally between the anvils of the test machine's , with the notch facing the approaching striker and centered precisely so the impact point aligns with the notch's , ensuring the longitudinal axis of the specimen is to the 's swing path. The is then raised and latched at a release angle of approximately 150° from the vertical position to achieve the required striking . The machine's safety interlocks are engaged to prevent premature release. Execution of the test involves releasing the pendulum latch, allowing it to swing freely under and strike the opposite side of the notch at a of about 5 m/s, fracturing the specimen in a three-point configuration. The continues unimpeded through the fracture plane to its maximum free swing height on the opposite side, with the entire motion captured to determine energy absorption. Following the impact, the absorbed energy is recorded directly from the machine's scale or digital readout, which measures the difference between the initial and the residual energy after , expressed in joules. The broken specimen halves are removed and visually inspected for surface features, such as cleavage or fibrous appearance, to note any qualitative aspects of mode. For reliable results, the test is repeated on at least three identical specimens under identical conditions to account for variability and compute meaningful averages. Safety protocols are integral throughout the process to protect operators from hazards associated with high-energy swings and extreme temperatures. Personnel must wear protective , including impact-resistant shields, safety glasses, gloves, and insulated handling tools for cryogenic specimens, while ensuring the pendulum is fully latched and the is locked during loading and unloading to prevent accidental strikes. Ventilation is maintained in areas involving to avoid asphyxiation risks from nitrogen displacement.

Specimen Requirements

Standard Dimensions and Preparation

The standard Charpy impact test specimen, as specified in ISO 148-1, is a rectangular bar measuring 55 mm in length with a square cross-section of 10 mm by 10 mm. A V-shaped notch is machined into the center of the specimen's length, perpendicular to the longitudinal axis, with a depth of 2 mm, an included angle of 45°, and a root radius of 0.25 mm. These dimensions ensure consistent stress concentration at the notch root, facilitating reproducible measurement of impact energy absorption. Specimens are prepared by from bulk material to achieve the required geometry, typically using milling or grinding to form the notch after rough cutting the bar. For heat-treated materials, final occurs after the heat treatment process to replicate service conditions, unless pre-heat-treatment is demonstrated to yield equivalent results. Surface finish must be free of defects such as , which can alter material properties; for steels, or metallographic examination may be used to verify surface integrity. For wrought materials like rolled plates or forgings, specimen orientation is critical and follows ISO 3785, distinguishing longitudinal () testing—where the notch is to the rolling direction—and transverse (T) testing—where the notch is parallel to the rolling direction—to account for anisotropic behavior. Specimens are marked on the face opposite the notch for identification, including orientation indicators (e.g., "" or "T") and test details, ensuring during handling. Quality control includes dimensional verification with tolerances as outlined in ISO 148-1 to maintain . The table below summarizes key dimensions and tolerances for the standard V-notch specimen:
DimensionNominal ValueTolerance
Length55 mm±0.5 mm
Width10 mm±0.1 mm
Thickness10 mm±0.1 mm
Notch depth2 mm±0.05 mm
Notch angle45°±1°
Notch root radius0.25 mm±0.02 mm
Distance from notch to end27.5 mm±0.25 mm
Optionally, specimens may undergo non-destructive testing, such as ultrasonic inspection, to detect internal defects like inclusions or cracks that could invalidate results, with rejection thresholds set based on project specifications (e.g., indications exceeding 1 mm in size).

Variations for Different Materials

Subsize specimens are employed in the Charpy impact test when material availability is limited, such as for thin sheets or weld zones, allowing evaluation of with reduced sample volumes. These specimens maintain the standard length of 55 mm but feature reduced cross-sections, for example, 10 mm width × 5 mm thickness, corresponding to half-size . To compare results to full-size tests, the measured absorbed of the subsize specimen is multiplied by AfAs\frac{A_f}{A_s} (where AfA_f is the full-size cross-sectional area and AsA_s the subsize area) to estimate the equivalent full-size , assuming proportional scaling based on surface area. Material-specific adaptations modify the notch geometry to suit the fracture behavior of non-metallic or composite materials. For plastics, the ISO 179 standard specifies U-notched specimens with a 1 mm radius and typically 2 mm depth to better capture ductile-brittle transitions in polymers, differing from the V-notch used for metals. In composites, deeper notches, such as 5 mm U-notches, are applied to account for anisotropic crack propagation and effects under impact. Miniature specimens with 3 mm thickness are particularly used for irradiated nuclear materials, enabling testing of embrittlement in steels while minimizing radiation exposure volume. Temperature adaptations extend the Charpy test to elevated conditions, with instrumented setups incorporating high-rate to measure dynamic responses up to 1000°C, as required for materials like tungsten-reinforced composites in high-heat environments. For small specimens, corrections address machine compliance, determined via low-blow elastic tests on unnotched samples to subtract pendulum deflection and yield accurate load-displacement curves. Non-metallic materials follow dedicated standards, such as ASTM D6110 for Charpy testing of plastics, which adapts procedures for brittle assessment in polymers.

Analysis of Results

Quantitative Measurements

The primary metric in the Charpy impact test is the absorbed impact EE, which quantifies the material's by measuring the required to the specimen. This is determined from the difference in the pendulum's before and after impact, calculated as E=mg(h1h2)E = m g (h_1 - h_2), where mm is the pendulum , gg is the (approximately 9.81 m/s²), h1h_1 is the initial release height, and h2h_2 is the height reached post-. In practice, the gross reading from the instrument dial or digital display is corrected for machine-specific losses to obtain the net absorbed by the specimen. Energy loss corrections account for in the bearings and air resistance (radiation), typically determined by performing a free swing without a specimen and subtracting this value (often 0.5–2 J) from the gross impact energy. Error analysis, including machine and , is limited to less than 2 J for verified instruments under standard conditions, ensuring reliable results through periodic against reference specimens. The combined standard u(E)u(E) incorporates contributions from specimen variability, , and instrument resolution, often computed as u(E)=s2n+ubias2+usystematic2u(E) = \sqrt{ \frac{s^2}{n} + u_{\text{bias}}^2 + u_{\text{systematic}}^2 }
Add your contribution
Related Hubs
User Avatar
No comments yet.