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Damage Characteristics and Residual Strength of Composite Sandwich Panels Impacted with and Without Compression LoadingThe results of an experimental study of the impact damage characteristics and residual strength of composite sandwich panels impacted with and without a compression loading are presented. Results of impact damage screening tests conducted to identify the impact-energy levels at which damage initiates and at which barely visible impact damage occurs in the impacted facesheet are discussed. Parametric effects studied in these tests include the impactor diameter, dropped-weight versus airgun-launched impactors, and the effect of the location of the impact site with respect to the panel boundaries. Residual strength results of panels tested in compression after impact are presented and compared with results of panels that are subjected to a compressive preload prior to being impacted.
Document ID
19980022721
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
McGowan, David M.
(NASA Langley Research Center Hampton, VA United States)
Ambur, Damodar R.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Publication Information
Publisher: American Inst. of Aeronautics and Astronautics
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-1998-207691
NAS 1.15:207691
AIAA Paper 98-1783
Report Number: NASA/TM-1998-207691
Report Number: NAS 1.15:207691
Report Number: AIAA Paper 98-1783
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: Long Beach, CA
Country: United States
Start Date: April 20, 1998
End Date: April 23, 1998
Sponsors: American Society of Mechanical Engineers, American Society of Civil Engineers, American Helicopter Society, Inc., American Society for Composites, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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