Previous Page  14 / 15 Next Page
Information
Show Menu
Previous Page 14 / 15 Next Page
Page Background

Анализ осевого вращательного движения рифленых кумулятивных облицовок

ISSN 0236-3941. Вестник МГТУ им. Н.Э. Баумана. Сер. Машиностроение. 2016. № 6

87

ANALYSIS OF FLUTED LINERS AXIAL ROTATION

S.S. Rassokha

rassokha@list.ru

S.V. Ladov

sm4-2009@mail.ru

A.V. Babkin

pc-os@bmstu.ru

Bauman Moscow State Technical University, Moscow, Russian Federation

Abstract

Keywords

The purpose of this work was to analyze the fluted liners axial

rotation by numerical and analytical methods. The study re-

vealed that pressure at the border between the liner and the

products of detonation depends on the pitch angle of the

oblique shock wave front. This is the cause for the rotation.

According to the pressure dependence on the angle between

the shock wave and the liner surface, we estimated the angular

velocity of the shaped charge jet. Influence of the liner material

properties and cross-section dimensions on jet angular velocity

also was evaluated. The results are in good agreement with

known experimental data

Shaped charge, shaped charge

jet, fluted liner, oblique shock

wave, rotation, spin-compen-

sation

REFERENCES

[1]

Walters W.P., Zukas J.A. Fundamentals of shaped charges. N.Y., John Wiley and Sons,

1989. 398 p.

[2]

Koch A., Jaggy P., Jaun W., Haller F. Study of spin-compensated shaped charges.

Proc.

19th Int. Symp. on Ballistics

. Interlaken (Switzerland), 2001. P. 1501–1508.

[3] Eichelberger R.J. Spin compensation.

Critical Review of Shaped Charge Information: Ballis-

tic Research Laboratories Report № 905

. Maryland, Aberdeen Proving Ground, 1959. 347 p.

[4]

Simon J., DiPersio R., Eichelberger R.J. Shaped charge performance with linear fluted

liners.

Ballistic Research Laboratories Memorandum Report № 1231

. Maryland, Aberdeen

Proving Ground, 1954. 38 p.

[5]

Cox C.M. Warhead mechanisms study.

Ballistic Research Laboratories Report № DA-33-

019-ORD-3697

. Maryland, Aberdeen Proving Ground, 1964. 147 p.

[6]

Kipp M.E., Martinez R.R., Hertel E.S., Baker E.L., Fuchs B.E., Chin C.L. Experiments

and

simulations of spinning shaped charges with fluted liners.

Proc. 18th Int. Symp. on Ballistics

.

San-Antonio (USA), 1999. Pp. 499–506.

[7]

Babkin A.V., Rassokha S.S., Ladov S.V., Odintsov V.A.

Fluted liners and spin-

compensation. Part 1, 2.

Izvestia RARAN

, 2013, no. 2, pp. 113–125 (in Russ.).

[8]

Babkin A.V., Rassokha S.S., Ladov S.V., Odintsov V.A.

Fluted liners and spin-

compensation. Part 2.

Izvestia RARAN

, 2013, no. 3, pp. 87–92 (in Russ.).

[9]

Smelikov V.G. Ustoichivost ogranichennoi kumulyacii [Stability of confined cumulation].

Moscow, Etnika Publ., 2016. 120 p.

[10]

Smelikov V.G., Sereda N.V., Lopatnikova T.V., Plotnikov A.A. “Stable” cumulation and

superplasticity, spinning of shear-formed shaped charge jets.

Boepripasi i visokoenergeticheskie

kondensirovannie sistemi,

2014, no. 1, pp. 32–77 (in Russ.).