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Advanced Computational Modeling Approaches for Shock Response PredictionMotivation: (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.
Document ID
20170007073
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
Authors
Derkevorkian, Armen
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kolaini, Ali R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Peterson, Lee
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 1, 2017
Publication Date
October 27, 2015
Subject Category
Mechanical Engineering
Computer Programming And Software
Meeting Information
Meeting: 2015 Aerospace Testing Seminar
Location: Los Angeles, CA
Country: United States
Start Date: October 27, 2015
End Date: October 29, 2015
Sponsors: Institute of Environmental Sciences and Technology
Distribution Limits
Public
Copyright
Other

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