Abstract

A first-principles-based model is presented for calculating the hole diameter resulting from the normal hypervelocity impact of a spherical aluminum projectile on a thin aluminum plate. One-dimensional shock theory is used to predict the creation and attenuation of Hugoniot pressures along the plate surface. Pressures are translated into the plate thickness by calculating intersecting positions of advancing shock fronts and centered-fan rarefaction waves. The radial position at which the shock pressure equals a predetermined value is defined to be the hole diameter. The model was calibrated by determining this critical value for aluminum-an-aluminum impacts using several hundred data points. A residuals analysis indicated some inherent problems with the model. Two empirical factors were added to account for thin plate and two-dimensional shock dissipation effects. The predictions of the adjusted model are shown to compare well with predictions of several empirical hole diameter models.

Highlights

  • The study of hypervelocity impacts against aluminum structures has its genesis in the early days of the space program

  • A one-dimensional formulation has been developed to predict the diameter of the hole created in a thin plate that has been impacted by a spherical projectile

  • This was accomplished by modeling the creation and attenuation of the Hugoniot impact pressure in a radial direction along the plate surface

Read more

Summary

Introduction

The study of hypervelocity impacts against aluminum structures has its genesis in the early days of the space program. There exists a need to develop an analytical hole diameter model for the high speed impact of a spherical projectile on a thin plate. In an attempt to address this need, this paper presents the development of an first-principles-based hole diameter model for the high speed impact of a spherical aluminum projectile on a thin aluminum target plate.

Results
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call