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Verifying the results of application software used to calculate the mechanical properties of materials is the subject of a new standard developed by ASTM International Committee E08 on Fatigue and Fracture. The new standard, E 2443, Guide for Verifying Computer-Generated Test Results Through the Use of Standard Data Sets, is under the jurisdiction of Subcommittee E08.03 on Advanced Apparatus and…
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Many structures, such as aircraft or other lightweight vehicles, are made from thin-ductile structural materials that exhibit low crack-front constraint, which allows for extensive plastic yielding of the material around a crack front. However, many current standards, such as E 399, Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials, or E 1820, Test Method…
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Representatives of ASTM International will visit the campus of Southern Methodist University (SMU) in Dallas, Texas, on the evening of Nov. 9, 2005, for an hour-long presentation to university students interested in the field of fatigue and fracture. The session will focus on the technical standards currently in use by this discipline as well as the ability of students and professionals to be…
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Executives from the Federal Aviation Administration (FAA) met with ASTM International members and staff at this years Airventure - a premier show and convention in the aviation world, hosted by the Experimental Aircraft Association (EAA). The briefing provided an update to the FAA on the status of ASTMs standards initiatives in the aviation sector. Among the representatives for the…
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For the first time, the Federal Aviation Administration (FAA) has used consensus standards for aircraft design, manufacturing, and maintenance with the acceptance of 15 standards developed by ASTM International Committee F37 on Light Sport Aircraft. The referenced documents, which have been worked on over the last two years, affect fixed-wing airplanes, powered parachutes, gyroplanes, lighter-…