ASTM E647-23b PDF
Standard Test Method for Measurement of Fatigue Crack Growth Rates
Standard Test Method for Measurement of Fatigue Crack Growth Rates
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 52
- Дата публикации:
- 15 ноября 2023 г.
- Издание:
- E647
- ICS:
- 77.040.10
SIGNIFICANCE AND USE 5.1 Fatigue crack growth rate expressed as a function of crack-tip stress-intensity factor range, da/dN versus ΔK, characterizes a material's resistance to stable crack extension under cyclic loading. Background information on the ration-ale for employing linear elastic fracture mechanics to analyze fatigue crack growth rate data is given in Refs (3) and (4). 5.1.1 In innocuous (inert) environments fatigue crack growth rates are primarily a function of ΔK and force ratio, R, or Kmax and R (Note 1). Temperature and aggressive environments can significantly affect da/dN versus ΔK, and in many cases accentuate R-effects and introduce effects of other loading variables such as cycle frequency and waveform. Attention needs to be given to the proper selection and control of these variables in research studies and in the generation of design data. Note 1: ΔK, Kmax, and R are not independent of each other. Specification of any two of these variables is sufficient to define the loading condition. It is customary to specify one of the stress-intensity parameters (ΔK or Kmax) along with the force ratio, R. 5.1.2 Expressing da/dN as a function of ΔK provides results that are independent of planar geometry, thus enabling exchange and comparison of data obtained from a variety of specimen configurations and loading conditions. Moreover, this feature enables da/dN versus ΔK data to be utilized in the design and evaluation of engineering structures. The concept of similitude is assumed, which implies that cracks of differing lengths subjected to the same nominal ΔK will advance by equal increments of crack extension per cycle. 5.1.3 Fatigue crack growth rate data are not always geometry-independent in the strict sense since thickness effects sometimes occur. However, data on the influence of thickness on fatigue crack growth rate are mixed. Fatigue crack growth rates over a wide range of ΔK have been reported to either increase, decrease, or remain unaffected as specimen... SCOPE 1.1 This test method2 covers the determination of fatigue crack growth rates from near-threshold (see region I in Fig. 1) to Kmax controlled instability (see region III in Fig. 1.) Results are expressed in terms of the crack-tip stress-intensity factor range (ΔK), defined by the theory of linear elasticity. 1.9 Special requirements for the various specimen configurations appear in the following order: The Compact Specimen Annex A1 The Middle Tension Specimen Annex A2 The Eccentrically-Loaded Single Edge Crack Tension Specimen Annex A3 1.10 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.11 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Abstract
Overview
ASTM E647-23b is the internationally recognized standard test method for the measurement of fatigue crack growth rates in materials. Established by ASTM International, this standard defines procedures for determining the rate at which a crack advances under cyclic loading-a critical parameter for characterizing a material’s resistance to fatigue failure. Results are expressed as the relationship between the fatigue crack growth rate (da/dN) and the crack-tip stress-intensity factor range (ΔK), which is fundamental for assessing structural component performance, predicting service life, and ensuring safety in engineering applications.
Key Topics
- Fatigue Crack Growth Rate (da/dN): Measures the rate at which a crack extends per loading cycle under repeated stress conditions.
- Crack-Tip Stress-Intensity Factor (ΔK): The key parameter, based on linear elastic fracture mechanics, representing the severity of the local stress field at the crack tip.
- Test Methods: Includes specific procedures and equipment for various specimen configurations, such as compact, middle-tension, and eccentrically-loaded single edge crack tension specimens.
- Influence of Environment and Loading Variables: Variables like temperature, environment (air, inert, or aggressive media), load ratio (R), frequency, and waveform can significantly impact fatigue crack growth rates.
- Geometry Independence: When properly applied, this standard allows comparison of results across different geometric configurations, making the data broadly transferable and valuable for material selection and design.
- Residual Stress and Crack Closure Effects: Addresses the implications of pre-existing stresses and crack tip shielding phenomena that can influence test results and their interpretation.
Applications
The ASTM E647-23b standard is widely utilized across industries where understanding fatigue behavior is essential:
- Aerospace: Ensures the structural integrity of airframes, engines, and critical components by evaluating growth rates of cracks under cyclic loading.
- Automotive: Supports development and validation of vehicles and components subject to dynamic stresses, contributing to improved durability and safety.
- Energy and Infrastructure: Assists in the assessment and maintenance planning of structures such as pipelines, bridges, and pressure vessels exposed to fluctuating loads.
- Materials Research and Development: Essential for comparing fatigue resistance among candidate alloys and optimizing material processes and heat treatments.
- Quality Assurance and Compliance: Provides a reliable basis for meeting strict industry requirements related to damage tolerance and lifecycle prediction.
Related Standards
Standard test methods and practices referenced or commonly used alongside ASTM E647 include:
- ASTM E399: Linear-Elastic Plane-Strain Fracture Toughness of Metallic Materials
- ASTM E1820: Measurement of Fracture Toughness
- ASTM E561: K₍R₎ Curve Determination
- ASTM E1012: Testing Frame and Specimen Alignment
- ASTM E8/E8M: Tension Testing of Metallic Materials
- ASTM E1823: Terminology Relating to Fatigue and Fracture Testing
The comprehensiveness and robustness of ASTM E647 make it foundational for fatigue crack growth testing. By standardizing the measurement methodology, this document ensures consistent, comparable, and accurate fatigue crack growth rate data, directly supporting safer and more durable engineering systems worldwide. When used in conjunction with related fracture mechanics standards, ASTM E647 enables engineers and researchers to predict structural integrity, inform maintenance schedules, and drive advancements in material science and technology.
Технические детали
- Технический комитет
- E08 - Fatigue and Fracture
- SKU
- ASTM E647-23b
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