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Impact damage in filament wound composite bottlesIncreasingly, composite materials are being used in advanced structural applications because of the significant weight savings they offer when compared to more traditional engineering materials. The higher cost of composites must be offset by the increased performance that results from reduced structural weight if these new materials are to be used effectively. At present, there is considerable interest in fabricating solid rocket motor cases out of composite materials, and capitalizing on the reduced structural weight to increase rocket performance. However, one of the difficulties that arises when composite materials are used is that composites can develop significant amounts of internal damage during low velocity impacts. Such low velocity impacts may be encountered in routine handling of a structural component like a rocket motor case. The ability to assess the reduction in structural integrity of composite motor cases that experience accidental impacts is essential if composite rocket motor cases are to be certified for manned flight. While experimental studies of the post-impact performance of filament wound composite motor cases haven been proven performed (2,3), scaling impact data from small specimens to full scale structures has proven difficult. If such a scaling methodology is to be achieved, an increased understanding of the damage processes which influence residual strength is required. The study described herein was part of an ongoing investigation of damage development and reduction of tensile strength in filament wound composites subjected to low velocity impacts. The present study, which focused on documenting the damage that develops in filament wound composites as a result of such impacts, included two distinct tasks. The first task was to experimentally assess impact damage in small, filament wound pressure bottles using x-ray radiography. The second task was to study the feasibility of using digital image processing techniques to assist in determining the 3-D distribution of damage from stereo x-ray pairs.
Document ID
19940019948
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Highsmith, Alton L.
(Alabama Univ. Tuscaloosa, AL, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1993
Publication Information
Publication: Alabama Univ., The 1993 NASA(ASEE Summer Faculty Fellowship Program
Subject Category
Composite Materials
Accession Number
94N24421
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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