TY - GEN
T1 - Method of characteristics simulation of interior ballistic processes of M1020 ignition cartridgein A 120-mm mortar system
AU - Kuo, Kenneth K.
AU - Acharya, Ragini
AU - Ferrara, Peter J.
AU - Moore, Jeffrey David
PY - 2005/12/1
Y1 - 2005/12/1
N2 - The objective of this study was to simulate the flame spreading and combustion processes in the ignition cartridge of a 120-mm mortar propulsion system under realistic firing conditions for performance improvements. In this work, theoretical modeling, numerical technique, and results of numerical simulation of the interior ballistic processes in the M1020 ignition cartridge of a 120-mm mortar system are presented. Modeling and simulation of the combustion processes in the granular propellant bed loaded with M48 ball propellants involves the solution of six coupled quasi-linear inhomogeneous hyperbolic partial differential equations (PDEs). These equations were formulated by applying the principles of conservation of mass, momentum and energy for condensed phase and gas phase in the granular propellant bed. In order to solve these equations for quantities of interest (i.e. pressure, propellant surface temperature, gas temperature, porosity, gas velocity, and propellant particle velocity), they were first converted to a system of ordinary differential equations (ODEs) using the method of characteristics (MOC). The MOC approach was selected because it introduces minimum numerical errors in converting the original system of PDEs into an equivalent system of ODEs. Calculated pressure-time traces showed axial pressure wave phenomena and compared closely with the measured pressure-time traces. The reason for the presence of pressure waves was found to be the non-uniform discharge of mass and energy of the combustion products from the vent holes of the flash tube.
AB - The objective of this study was to simulate the flame spreading and combustion processes in the ignition cartridge of a 120-mm mortar propulsion system under realistic firing conditions for performance improvements. In this work, theoretical modeling, numerical technique, and results of numerical simulation of the interior ballistic processes in the M1020 ignition cartridge of a 120-mm mortar system are presented. Modeling and simulation of the combustion processes in the granular propellant bed loaded with M48 ball propellants involves the solution of six coupled quasi-linear inhomogeneous hyperbolic partial differential equations (PDEs). These equations were formulated by applying the principles of conservation of mass, momentum and energy for condensed phase and gas phase in the granular propellant bed. In order to solve these equations for quantities of interest (i.e. pressure, propellant surface temperature, gas temperature, porosity, gas velocity, and propellant particle velocity), they were first converted to a system of ordinary differential equations (ODEs) using the method of characteristics (MOC). The MOC approach was selected because it introduces minimum numerical errors in converting the original system of PDEs into an equivalent system of ODEs. Calculated pressure-time traces showed axial pressure wave phenomena and compared closely with the measured pressure-time traces. The reason for the presence of pressure waves was found to be the non-uniform discharge of mass and energy of the combustion products from the vent holes of the flash tube.
UR - http://www.scopus.com/inward/record.url?scp=77956828896&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=77956828896&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:77956828896
SN - 9781567002393
T3 - Advancements in Energetic Materials and Chemical Propulsion
SP - 621
EP - 642
BT - Advancements in Energetic Materials and Chemical Propulsion
T2 - 6th International Symposium on Special Topics in Chemical Propulsion: Advancements in Energetic Materials and Chemical Propulsion, ISICP 2006
Y2 - 8 March 2005 through 11 March 2005
ER -