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Low and high velocity impact response of thick hybrid compositesThe effects of low and high velocity impact on thick hybrid composites (THC's) were experimentally compared. Test Beams consisted of CFRP skins which were bonded onto an interleaved syntactic foam core and cured at 177 C (350 F). The impactor tip for both cases was a 16 mm (0.625 inch) steel hemisphere. In spite of the order of magnitude difference in velocity ranges and impactor weights, similar relationships between impact energy, damage size, and residual strength were found. The dependence of the skin compressive strength on damage size agree well with analytical open hole models for composite laminates and may enable the prediction of ultimate performance for the damaged composite, based on visual inspection.
Document ID
19940012364
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hiel, Clement
(NASA Ames Research Center Moffett Field, CA, United States)
Ishai, Ori
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 31, 1993
Publication Information
Publication: Texas Univ., Effect of Impact Damage and Open Hole on Compressive Strength of Hybrid Composite Laminates
Subject Category
Composite Materials
Accession Number
94N16837
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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