A comparative study between experimental results and numerical predictions of multi-wall structural response to hypervelocity impactOver the last three decades, multiwall structures have been analyzed extensively, primarily through experiment, as a means of increasing the protection afforded to spacecraft structure. However, as structural configurations become more varied, the number of tests required to characterize their response increases dramatically. As an alternative, numerical modeling of high-speed impact phenomena is often being used to predict the response of a variety of structural systems under impact loading conditions. This paper presents the results of a preliminary numerical/experimental investigation of the hypervelocity impact response of multiwall structures. The results of experimental high-speed impact tests are compared against the predictions of the HULL hydrodynamic computer code. It is shown that the hypervelocity impact response characteristics of a specific system cannot be accurately predicted from a limited number of HULL code impact simulations. However, if a wide range of impact loadings conditions are considered, then the ballistic limit curve of the system based on the entire series of numerical simulations can be used as a relatively accurate indication of actual system response.
Document ID
19920056055
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schonberg, William P. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Peck, Jeffrey A. (Alabama, University Huntsville, United States)