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A Review of Recent Developments in the Holographic Observation of Disbonds Picatinny Arsenal, U. S. Army

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Kisatsky, Paul J., author.
Conference Name:
1974 Automotive Engineering Congress and Exposition (1974-02-25 : Detroit, Michigan, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1974
Summary:
Holographic techniques have been employed to observe nondestructively the presence of disbonds or bond degradation in adhesives of thin and thick laminates. It is shown that when panels of honeycomb aircraft skin are exposed to prolonged humidity, the time history of bond weakening can be holographically observed as the humidity attack proceeds inward from the edges. While heat stressing is suitable to the holographic observation of disbonds in "thin" laminates, it generally fails in thick structures. A second technique of exciting resonance patterns of disbonds and observing them with time-averaged holography is suitable for use with thicker materials. Various mode patterns of disbonds have been observed in "thick" laminates of the ceramic-fiberglass epoxy composites considered for use in applications such as missile radomes
Notes:
Vendor supplied data
Publisher Number:
740258
Access Restriction:
Restricted for use by site license

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