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Image
Published: 01 January 2000
Image
in Fatigue, Creep Fatigue, and Thermomechanical Fatigue Life Testing
> Mechanical Testing and Evaluation
Published: 01 January 2000
Image
Published: 01 January 2001
Fig. 2 General arrangement of specimens within a controlled environmental chamber for thermal conductivity measurements using the ASTM C 177 method. This is known as the guarded hot-plate method.
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Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003314
EISBN: 978-1-62708-176-4
... fatigue testing machines and bending fatigue machines. Load cells, grips and alignment devices, extensometry and strain measuring devices, environmental chambers, graphic recorders, furnaces, and heating systems of ancillary equipment are discussed. The article presents technologies available...
Abstract
This article describes the phenomena of crack initiation and early growth. It examines specimen design and preparation as well as the apparatus used in crack initiation testing. The article provides descriptions of the various commercially available fatigue testing machines: axial fatigue testing machines and bending fatigue machines. Load cells, grips and alignment devices, extensometry and strain measuring devices, environmental chambers, graphic recorders, furnaces, and heating systems of ancillary equipment are discussed. The article presents technologies available to accomplish closed loop control of materials testing systems in performing standard materials tests and for the development of custom testing applications. It explores the advanced software tools for materials testing. The article includes a description of baseline isothermal fatigue testing, creep-fatigue interaction, and thermomechanical fatigue. The effects of various variables on fatigue resistance and guidelines for fatigue testing are also presented.
Image
Published: 01 January 2000
Book Chapter
Book: Fractography
Series: ASM Handbook Archive
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000629
EISBN: 978-1-62708-181-8
... in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were tested at moisture conditions designed not to alter their conditioning, and at the temperatures noted.) (L. Clements, San Jose State University, and J.C. Liu, Cornell University) Fig. 1297 Fracture surface...
Abstract
This article is an atlas of fractographs that helps in understanding the causes and mechanisms of fracture of a type of resin-matrix composites, carbon-epoxy composites. The fractographs illustrate the fracture modes found in composite prepregs, composite panels, solid rocket motor nozzles, and tension, flexural, compressive, and shear loadings.
Image
Published: 01 January 2005
Fig. 5 Typical examples of heating methods for load-frame tension testing. (a) Induction heating. (b) Environmental chamber. (c) Split-furnace setup
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Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003267
EISBN: 978-1-62708-176-4
..., the test machine must be equipped with a temperature-controlled environmental chamber. One consideration for the suitability of the machine for low-temperature tests is the ease with which a low-temperature environmental chamber can be implemented. The physical characteristics of the test machine come...
Abstract
This article provides a discussion on the mechanical properties of metals, ceramics, and polymers and fiber-reinforced polymer composites at low temperatures. It reviews the factors to be considered in tensile and compression testing of these materials. The article details the equipment used for low-temperature tensile and compression tests with illustrations. It concludes with a discussion on the various test methods and their ASTM standard for compression and tension testing.
Image
Published: 01 January 1987
at 60 °C (140 °F) and 60% relative humidity for at least 2 months and then placed in a drawer in the laboratory for several months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative
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Image
Published: 01 January 1987
at 60 °C (140 °F) and 60% relative humidity for at least 2 months and then placed in a drawer in the laboratory for several months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative
More
Image
Published: 01 January 1987
, having been placed after drying in a chamber at 60 °C (140 °F) and 60% relative humidity for at least 2 months and then placed in a drawer in the laboratory for several months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental
More
Image
Published: 01 January 1987
after drying in a chamber at 60 °C (140 °F) and 60% relative humidity for at least 2 months and then placed in a drawer in the laboratory for several months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140
More
Image
Published: 01 January 1987
months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were tested at moisture conditions designed not to alter their conditioning, and at the temperatures
More
Image
Published: 01 January 1987
in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were tested at moisture conditions designed not to alter their conditioning, and at the temperatures noted.) (L. Clements, San Jose State University and P.R. Lee, United Technologies)
More
Image
Published: 01 January 1987
testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were tested at moisture conditions designed not to alter their conditioning, and at the temperatures noted.) (L
More
Image
Published: 01 January 1987
placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were tested at moisture conditions designed not to alter their conditioning, and at the temperatures noted.) (L. Clements, San Jose State University, and P.R. Lee, United Technologies)
More
Image
Published: 01 January 1987
in the laboratory for several months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were tested at moisture conditions designed not to alter their conditioning
More
Image
Published: 01 January 1987
in a drawer in the laboratory for several months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were tested at moisture conditions designed not to alter
More
Image
Published: 01 January 1987
months and then placed in a drawer in the laboratory for several months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were tested at moisture conditions
More
Image
Published: 01 January 1987
% relative humidity for at least 2 months and then placed in a drawer in the laboratory for several months before testing. “Wet” specimens had about 1.5 to 2.0 wt% moisture, having been placed for several months in an environmental chamber at 60 °C (140 °F) and 100% relative humidity. The composites were
More
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