The revolving barrel gun is the principal component of the close-in weapons system (CIWS) that provides important terminal defense against anti-ship cruise missiles that have penetrated fleet defenses. The muzzle flow field of the revolving barrel firing is extraordinarily complex. The 3D computational model was formulated to illustrate the details of the flow field produced by the revolving barrel gun firing. The algorithm of a second order monotone upstream-centered schemes (MUSCL) approach with the advection upstream splitting method (AUSM) solver was used to simulate the high pressure muzzle flow field. The interior ballistic process was coupled with the simulation. The predicted muzzle velocity and maximum bore pressure were in good agreement with those measured in gun firing. Moreover, the muzzle flow field was obtained during the revolving barrel firing and was subsequently analyzed. The maximum lateral velocity of the first and second projectile fired was about 1.6 and 3.8 m/s.

References

1.
Apte
,
A.
, and
Rendon
,
R.
,
2009
, “
A Diagnostic Approach to Weapon System Lifecycle Support: The Phalanx Close-In Weapon System
,” Paper No. ADA494595.
2.
Watanabe
,
R.
,
Fujii
,
K.
, and
Higashino
,
F.
,
1997
, “
Three-Dimensional Computation of the Flow Induced by a Projectile Overtaking a Shock Wave
,” AIAA Paper No. 97-1840.
3.
Aibarow
,
A. V.
,
Babayev
,
D. B.
, and
Mironov
,
A. A.
,
2002
, “
Numerical Simulation of 3D Muzzle Brake and Missile Launcher Flow Field in the Presence of Movable Objects
,”
20th International Symposium in Ballistics
,
Orlando, FL
, September 23–27, pp.
226
232
.
4.
Merlen
,
A.
, and
Dyment
,
A.
,
1991
, “
Similarity and Asymptotic Analysis for Gun-Firing Aerodynamics
,”
J. Fluid Mech.
,
225
, pp.
497
528
.10.1017/S0022112091002148
5.
Cayzac
,
R.
,
Carette
,
E.
, and
Alziary de Roquefort
,
T.
,
2008
, “
3D Unsteady Intermediate Ballistics Modeling: Muzzle Brake and Sabot Separation
,”
24th International Symposium on Ballistics
,
New Orleans, LA
, September 22–26, pp.
423
430
.
6.
Cayzac
,
R.
,
Carette
,
E.
,
Alziary de Roquefort
, T.
,
Renard
,
F. X.
,
Roux
,
D.
,
Patry
,
J. N.
, and
Balbo
,
P.
,
2010
, “
Advanced 120 mm Lightweight Tank Demonstrator: Direct Modeling of the Interior, Intermediate and Exterior Ballistic as Well as the Weapon System Environment
,”
25th International Symposium on Ballistics
,
Beijing, China
, May 17–21, pp.
505
511
.
7.
Cler
,
D. L.
,
Chevaugeon
,
N.
,
Shephard
,
M. S.
,
Flaherty
,
J. E.
, and
Remacle
,
J.-F.
,
2003
, “
Computational Fluid Dynamics Application to Gun Muzzle Blast: A Validation Case Study
,” Technical Report ARCCB-TR-03011.
8.
Sakamoto
,
K.
,
Matsunaga
,
K.
,
Fukushima
,
J.
, and
Tanaka
,
A.
,
2001
, “
Numerical Analysis of the Propagating Blast Wave in a Firing Range
,”
19th International Symposium on Ballistics
,
Interlaken, Switzerland
, May 7–11, pp.
245
251
.
9.
Cayzac
,
R.
,
Carette
,
E.
,
Alziary de Roquefort
,
T.
,
Bidorini
,
P.
,
Bret
,
E.
,
Delusier
,
P.
, and
Secco
,
S.
,
2005
, “
Unsteady Intermediate Ballistics: 2D and 3D CFD Modeling: Applications to Sabot Separation
,”
22nd International Symposium on Ballistics
,
Vancouver, Canada
, November 14–18, pp.
398
404
.
10.
Kurbatskii
,
K. A.
, and
Montanari
,
F.
,
2007
, “
Numerical Blast Wave Identification and Tracking Using Solution-Based Mesh Adaptation Approach
,”
AIAA
Paper No. 2007-4188. 10.2514/6.2007-4188
11.
Yamashita
,
S.
,
Chen
,
C. G.
,
Takahashi
,
K.
, and
Xiao
,
F.
,
2008
, “
Large Scale Numerical Simulations for Multi-Phase Fluid Dynamics With Moving Interfaces
,”
Int. J. Comput. Fluid Dyn.
,
22
(
6
), pp.
405
410
.10.1080/10618560802199691
12.
Mirsajedi
,
S. M.
,
Karimian
,
S. M. H.
, and
Mani
,
M.
,
2006
, “
A Multi-Zone Moving Mesh Algorithm for Simulation of Flow Around a Rigid Body With Arbitrary Motion
,”
ASME J. Fluids Eng.
,
128
(
3
), pp.
297
304
.10.1115/1.2170124
13.
Carlucci
,
D.
,
Cordes
,
J.
,
Morris
,
S.
, and
Gast
,
R.
,
2006
, “
Muzzle Exit (Set Forward) Effects on Projectile Dynamics
,” Paper No. AD-E403 082.
14.
Jin
,
Z. M.
,
2004
,
Interior Ballistics of Guns
,
Beijing Institute of Technology Press
,
Beijing, China
.
15.
Blazek
,
J.
,
2001
,
Computational Fluid Dynamics: Principles and Applications
,
Elsevier
,
New York
, pp.
81
96
.
16.
Liou
,
M. S.
,
2003
, “
A Further Development of the AUSM+ Scheme Towards Robust and Accurate Solutions for All Speeds
,”
AIAA
Paper No. 2003-4116. 10.2514/6.2003-4116
17.
Langer
,
S.
, and
Li
,
D.
,
2011
, “
Application of Point Implicit Runge-Kutta Methods to Inviscid and Laminar Flow Problems Using AUSM and AUSM(+) Upwinding
,”
Int. J. Comput. Fluid Dyn.
,
25
(
5
), pp.
255
269
.10.1080/10618562.2011.590801
18.
Yu
,
W.
, and
Zhang
,
X. B.
,
2010
, “
Aerodynamic Analysis of Projectile in Gun System Firing Process
,”
ASME J. Appl. Mech.
,
77
(
5
), p.
051406
.10.1115/1.4001559
19.
Li
,
K. J.
, and
Zhang
,
X. B.
,
2011
, “
Multi-Objective Optimization of Interior Ballistic Performance Using NSGA-II
,”
Propellants, Explos., Pyrotech.
,
36
, pp.
282
290
.10.1002/prep.201000027
20.
Zhang
,
X. B.
, and
Wang
,
Y. Z.
,
2010
, “
Analysis of Dynamic Characteristics for Rarefaction Wave Gun During the Launching
,”
ASME J. Appl. Mech.
,
77
(
5
), p.
051601
.10.1115/1.4001289
You do not currently have access to this content.