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BS EN 2155-13:1993 Test methods for transparent materials for aircraft glazing - Part 13. Determination of temperature at deflection under load

Description Printed version of this is available at library. To request, please e-mail to referencepk@usm.my and include a copy of this record in your e-mail. Abstract This standard specifies a procedure for determining the temperature at which an arbitrary deformation occurs when the specimens are subjected to arbitrary bending loads, under conditions of continually rising temperatures. The procedure applies to materials in sheet form in thicknesses > 3 mm. It does not apply to stretched/pressed (homogenous) acrylic materials. Definitions For the purpose of this test the temperature of deflection under load is that temperature (attained during conditions of steady increase of temperature) at which a specimen of the material exhibits a specified deflection.

Contributor(s): MAR - Data Entry Person Primary Item Type: British Standard Identifiers: ICS 49.045 Structure and structure elements ISBN 0580220664 Language: English Subject Keywords: Sheet materials; Plastics; Deflection tests; Glazing; Transparency; Thermal testing; Test equipment; Specimen preparation; Air transport engineering; Temperature measurement; Testing conditions; Aircraft components; Glass; Thickness First presented to the public: 1/10/2024 Original Publication Date: 4/15/1993 Previously Published By: British Standards Institution Place Of Publication: London, United Kingdom Citation: Extents: Number of Pages - 8 License Grantor / Date Granted:   / ( View License ) Date Deposited 2024-01-10 11:38:46.709 Submitter: Muhamad Azmil Ramli

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