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Dynamic Crush Characterization of IceDuring the space shuttle return-to-flight preparations following the Columbia accident, finite element models were needed that could predict the threshold of critical damage to the orbiter's wing leading edge from ice debris impacts. Hence, an experimental program was initiated to provide crushing data from impacted ice for use in dynamic finite element material models. A high-speed drop tower was configured to capture force time histories of ice cylinders for impacts up to approximately 100 ft/s. At low velocity, the force-time history depended heavily on the internal crystalline structure of the ice. However, for velocities of 100 ft/s and above, the ice fractured on impact, behaved more like a fluid, and the subsequent force-time history curves were much less dependent on the internal crystalline structure.
Document ID
20060007589
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Fasanella, Edwin L.
(Army Research Lab. Hampton, VA, United States)
Boitnott, Richard L.
(Army Research Lab. Hampton, VA, United States)
Kellas, Sotiris
(General Dynamics Advanced Information Systems United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2006
Subject Category
Air Transportation And Safety
Report/Patent Number
ARL-TR-3753
L-19225
NASA/TM-2006-214278
Report Number: ARL-TR-3753
Report Number: L-19225
Report Number: NASA/TM-2006-214278
Funding Number(s)
WBS: WU 377816.06.03.03.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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