The given article presents the conducted calculation and experimental study on destruction of heat-resistant coating material of an aircraft in the process of high-speed interaction of the steel spherical projectile. The projectile is imitating a meteoric particle. The study was conducted in the wide range of velocities. The mathematical behavioral model of heat-resistant coating under high-speed impact was developed. The interaction of ameteoric particle with an element of the protective structure has especially individual character and depends on impact velocity and angle, materials of the interacting solids
AbstractMonolithic, porous, thermal protection systems were used heavily on the Apollo command modul...
The problem of protecting spacecraft from cosmic dust has recently come to the fore. There is still ...
High velocity solid particle erosion may cause severe damage and high wear rates in materials used f...
The given article presents the conducted calculation and experimental study on destruction of heat-r...
The paper presents a calculation-experimental study on high-speed interaction of the metal projectil...
This paper discusses the interactions of barriers with a spherical impactor and the character of pos...
In this work the influence of the characteristics ofthematerial ofthe striker (cumulative jet or pr...
The results of numerical simulations of a compact steel impactor with the aluminum porous shields un...
The process of high-speed impact of projectiles against targets of finite thickness is experimentall...
In this paper we present calculating and experimental study of high-speed interaction between explos...
This study deals with the effect of complex material made from (Kevlar29, Honeycomb Aluminium and...
Crater characteristics of 11 metal alloys under hypervelocity impact including effects of projectile...
A collision process of a high speed debris with a spherical or cylindrical shape against a thin plat...
AbstractPorous-ceramic, thermal protection systems were used heavily on the Orbiter, and they are cu...
In this paper we consider issues related to numerical modelling of processes of high-speed impact ef...
AbstractMonolithic, porous, thermal protection systems were used heavily on the Apollo command modul...
The problem of protecting spacecraft from cosmic dust has recently come to the fore. There is still ...
High velocity solid particle erosion may cause severe damage and high wear rates in materials used f...
The given article presents the conducted calculation and experimental study on destruction of heat-r...
The paper presents a calculation-experimental study on high-speed interaction of the metal projectil...
This paper discusses the interactions of barriers with a spherical impactor and the character of pos...
In this work the influence of the characteristics ofthematerial ofthe striker (cumulative jet or pr...
The results of numerical simulations of a compact steel impactor with the aluminum porous shields un...
The process of high-speed impact of projectiles against targets of finite thickness is experimentall...
In this paper we present calculating and experimental study of high-speed interaction between explos...
This study deals with the effect of complex material made from (Kevlar29, Honeycomb Aluminium and...
Crater characteristics of 11 metal alloys under hypervelocity impact including effects of projectile...
A collision process of a high speed debris with a spherical or cylindrical shape against a thin plat...
AbstractPorous-ceramic, thermal protection systems were used heavily on the Orbiter, and they are cu...
In this paper we consider issues related to numerical modelling of processes of high-speed impact ef...
AbstractMonolithic, porous, thermal protection systems were used heavily on the Apollo command modul...
The problem of protecting spacecraft from cosmic dust has recently come to the fore. There is still ...
High velocity solid particle erosion may cause severe damage and high wear rates in materials used f...