A phenomenological high strain rate model with failure for ice
By K. Carney, David J. Benson, Paul Dubois, Ryan Lee. 2006
180 citations recorded by the source corpus.
Modeling the high velocity impact of ice was a requirement in the safety calculations for the return-to-flight of the Space Shuttle on July 26, 2005. Ice, however, is not a common structural material and commercial finite element programs did not have any appropriate models. A phenomenological model with failure was developed to match experimental ballistic tests. The model has a relatively small number of material constants, most of which have been measured experimentally. A description of the model and comparisons of calculations to experiments are presented.
Subfields: Aerospace Engineering, Atmospheric Science, Civil and Structural Engineering
View Paper: https://www.semanticscholar.org/paper/77f8326e535aaf622070b53873c55a3bd89c1b8e
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In Aerospace Engineering
In Civil and Structural Engineering
Citations in the corpus
- On erosion issues associated with the leading edge of wind turbine blades (2013, methodology): “Carney et al [71] summarized that polycrystalline and single crystal ice exhibit strain rate sensitivity from 10−8 s−1 to 10−2 s−1 and that single crystal ice has also been shown to be rate sensitive in the range of ∼100 to 103.”
- High strain-rate behavior of ice under uniaxial compression (2009, unknown): “Contents lists available at ScienceDirect International Journal of Solids and Structures journal homepage: www.elsevier .com/ locate / i jsols t r High strain-rate behavior of ice under uniaxial compression Mostafa Shazly a, Vikas Prakash a,*, Bradley A. Lerch b a Department of Mechanical and Aerosp”