The multilevel stepped-wall chamber is designed to study the combustion stability control mechanism of the bulk-loaded liquid propellant gun (BLPG). The cold state experiment of the interaction of the high speed gas jet with liquid medium is conducted by means of high speed digital camera system. The simulated small caliber bulk-loaded liquid propellant combustion propulsion device is designed to study the effect of the stepped-wall chamber size on the combustion stability. The experimental results indicate that, the stepped-wall structure can restrain the expansion randomness of the Taylor cavity and leads smooth expansion at each step. In 4 stepped-wall chamber with ΔD/L = 3/40, the interior ballistic performance of BLPG is stable and the consistency of the p-t curves is good. Two-dimensional unsteady model is developed based on the BLPG combustion propulsion experiment. The numerical simulation results coincide well with the experiment.

References

1.
Morrison
,
W. F.
,
Knapton
,
J. D.
, and
Bulman
,
M. J.
, 1988, “
Liquid Propellant Guns
,”
Prog. Astronaut. Aeronaut.
pp.
431
471
.
2.
Talley
,
R. L.
, 1994, “
Interior Ballistic Process Control Using Mechanical Concepts Medium Caliber Bulk-loaded LP Guns
,”
Proceedings 31st JANNAF Combustion Subcommittee Meeting
, CPIA Publication 620, Vol.
I
, pp.
303
312
.
3.
Bracuti
,
A. J.
, and
Chiu
,
D. S.
, 1995, “
Advanced Propulsion Concept: Step Chamber for Bulk Loaded LP Gun
,” ADA 296691.
4.
Talley
,
R. L.
, and
Owczarczak
,
J. A.
, 1994, “
Investigation of Bulk-Loaded Liquid Propellant Gun Concepts
,” ARL-CR-127, Aberdeen: U.S. ARL.
5.
Talley
,
R. L.
, 1995, “
Exploration of Mechanical Concepts to Achieve Interior Ballistic Process Control in Bulk-Loaded Liquid Propellant Guns
,”
Proceedings of the 32nd JANNAF Combustion Subcommittee Meeting
, CPIA Publication 631, Vol.
I
.
6.
Rocenberger
,
T. E.
, and
Knapton
,
J. D.
, 1995, “
Test Results From a 37-mm Segmented-Chamber Bulk-Loaded Propellant Gun
,” ARL-TR-871.
7.
Knapton
,
J. D.
,
DeSpirito
,
J.
,
Rosenberger
,
T. E.
, et al.
, 1995, “
Correlation of Igniter Output to Early Combustion Chamber Pressure Rise in Bulk-loaded Liquid Propellant Gun
,”
Proceedings 32nd JANNAF Combustion Subcommittee Meeting
, CPIA Publication 631, Vol.
I
.
8.
Talley
,
R. L.
, 1995, “
Interior and Exterior Testing of Bulk Loaded Propellant in a 40 mm Gun
,” Report D48-95-001,
U.S. Army Armament Research. Development and Engineering Center Picatinny Arsenal
, NJ.
9.
Talley
,
R. L.
, and
Owczarczak
,
J. A.
, 1997, “
Investigation of Bulk-Loaded Liquid Propellant Gun Concepts
,” ARL-CR-335.
10.
Burnett
,
W. M.,
1976, “
An Interior Ballistic Model for Liquid Propellant Guns
,” TR-444, Aberdeen: U.S. Naval Ordnance Station.
11.
Edelman
,
R. B.
, and
Hogge
,
H. D.
, 1976, “
A Transient Quasi-One-Dimensional Model of the Interior Ballistic Process for Non-Hypergolic Liquid Bi-Propellant Guns
,” RDA-TR-8700-001.
12.
Edelman
,
R. B.
,
Phillips
,
G. T.
, and
Wang
,
T. S.
, 1983, “
Analysis of Interior Ballistics Processes of Bulk-Loaded Liquid Propellant Guns
,” ARL 83-048.
13.
Kuo
,
K. K.
,
Cheung
,
F. B.
, and
Chen
J. L.
, 1989, “
A Multi-Phase Multi-Dimensional Transient Bulk-Loaded Liquid Propellant Gun Model
,”
Proceedings of the 11th International Symposium on Ballistics
.
14.
Madabhushi
,
R. K.
,
Hosangadi
,
A.
,
Sinha
,
N.
, and
Dash
,
S. M.
, 1994, “
Large Eddy Simulation Studies of Vortex-Shedding With Application to LPG Instabilities Using the CRAFT Navier-Stokes Codes
,” TR-120.
15.
Despirito
,
J.
, 1996, “
CFD Analysis of the Interior Ballistics of the Bulk-Load Liquid Propellant
,” AIAA 96-3079.
16.
Despirito
,
J.
, 2001, “
Interior Ballistic Simulations of the Bulk-Loaded Liquid Propellant Gun
,” ARL-TR-2316.
17.
Yu
,
Y. G.
,
Chang
,
X. X.
,
Zhou
,
Y. H,
, and
Mang
,
S. S.
, 2008, “
Experiment and Numerical Simulation of Combustion and Propulsion of Bulk-Loaded Energetic Liquid
,”
J. Eng. Thermophys.
,
29
(
3
), pp.
531
534
.
You do not currently have access to this content.