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NASA NTRS ยท 19900015881

Method of insetting predesigned disbond areas into composite laminates

Abstract

This invention is a process for producing composite laminates containing interlaminar disbonds of controlled sizes, shapes, and positions within a composite structure. A composite layer is provided for later inclusion within a laminate. The surfaces of this composite layer are solvent cleaned and sandblasted, except in desired disbond areas, which are coated with a releasing surface. A template to mask the bond areas is employed to obtain disbond areas of controlled shapes and sizes. The resulting composite layer is then used in the subsequent manufacture of a laminate, whereby faulty adhesion in the laminate can be studied with prior knowledge of the size, shape, and location of the disbond areas.

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BibTeXRIS

Dickerson, George E.. 1990-05-08. Method of insetting predesigned disbond areas into composite laminates. https://ntrs.nasa.gov/citations/19900015881

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