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Shock propagation in a target subjected to hypervelocity impact of an incident projectile

T. S. Fu

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Abstract

A hydrodynamic model, based on shock diffraction theory and the q u a s i -s i m i l a r i t y solutions of blast wave theory, i s developed t o d e s c r i b e the shock profile h i s t o r y in a m e t a l t a r g e t on which a hypervelocity m e t a l projectile impacts.A finite difference integration of the resultant method of c h a r a c t e r i s t i c solution i s used to obtain n u m e r i c a l r e s u l t s .A n u m e r i c a l example of aluminum impacting on aluminum at a velocity of 20 k m / s e c i s presented.The comparison with the d i r e c t n u m e r i c a l r e s u l t s shows a good agreement f o r the c a s e selected.

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A hydrodynamic model, based on shock diffraction theory and the q u a s i -s i m i l a r i t y solutions of blast wave theory, i s developed t o d e s c r i b e the shock profile h i s t o r y in a m e t a l t a r g e t on which a hypervelocity m e t a l projectile impacts.A finite difference integration of the resultant method of c h a r a c t e r i s t i c solution i s used to obtain n u m e r i c a l r e s u l t s .A n u m e r i c a l example of aluminum impacting on aluminum at a velocity of 20 k m / s e c i s presented.The comparison with the d i r e c t n u m e r i c a l r e s u l t s shows a good agreement f o r the c a s e selected.

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Available abstract

A hydrodynamic model, based on shock diffraction theory and the q u a s i -s i m i l a r i t y solutions of blast wave theory, i s developed t o d e s c r i b e the shock profile h i s t o r y in a m e t a l t a r g e t on which a hypervelocity m e t a l projectile impacts.A finite difference integration of the resultant method of c h a r a c t e r i s t i c solution i s used to obtain n u m e r i c a l r e s u l t s .A n u m e r i c a l example of aluminum impacting on aluminum at a velocity of 20 k m / s e c i s presented.The comparison with the d i r e c t n u m e r i c a l r e s u l t s shows a good agreement f o r the c a s e selected.

Key concepts: Hypervelocity, Projectile, Shock (circulatory), Physics, Mechanics, Aerospace engineering, Engineering, Medicine

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