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NASA NTRS · 20170007073

Advanced Computational Modeling Approaches for Shock Response Prediction

Abstract

Motivation: (1) The activation of pyroshock devices such as explosives, separation nuts, pin-pullers, etc. produces high frequency transient structural response, typically from few tens of Hz to several hundreds of kHz. (2) Lack of reliable analytical tools makes the prediction of appropriate design and qualification test levels a challenge. (3) In the past few decades, several attempts have been made to develop methodologies that predict the structural responses to shock environments. (4) Currently, there is no validated approach that is viable to predict shock environments overt the full frequency range (i.e., ~100 Hz to 10 kHz). Scope: (1) Model, analyze, and interpret space structural systems with complex interfaces and discontinuities, subjected to shock loads. (2) Assess the viability of a suite of numerical tools to simulate transient, non-linear solid mechanics and structural dynamics problems, such as shock wave propagation.

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BibTeXRIS

Derkevorkian, Armen, Kolaini, Ali R., Peterson, Lee. 2015-10-27. Advanced Computational Modeling Approaches for Shock Response Prediction. https://ntrs.nasa.gov/citations/20170007073

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