• Title/Summary/Keyword: Interior Ballistics

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Development of Numerical Model for Igniter and Study on Initial Ignition of Interior Ballistics (강내탄도의 점화기 해석 모델 개발 및 초기 점화 연구)

  • Sung, Hyung-Gun;Jang, Jin-Sung;Choi, Dong-Whan;Roh, Tae-Seong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.953-961
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    • 2011
  • A numerical model of the igniter for the interior ballistics has been developed combining the lumped parameter model with the theoretical equation of the orifice. With the developed model of the igniter, the numerical study on characteristics of the interior ballistics according to the igniter configuration in terms of the igniter length, the side hole diameter, and the distribution of side holes has been conducted. As results of the calculation of the pressure difference between the breech and shot base, the low frequency oscillations have been influenced by the igniter length, while the high frequency oscillations have been affected by the side hole diameter and the distribution of side holes.

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Analysis of Elements Influencing on Performance of Interior Ballistics (강내탄도의 성능 영향 요소 분석)

  • Sung, Hyung-Gun;Yoo, Seung-Young;Lee, Sang-Bok;Choi, Dong-Whan;Roh, Tae-Seong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.4
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    • pp.16-24
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    • 2013
  • The analysis of performance and internal flow according to various numerical models for interior ballistics has been conducted. The initial flow has been mainly affected by the drag model of propellants and their drag degradation reduces oscillations of differential pressure between the breech and the shot base. Models of Nusselt number haven't influenced the major performance of interior ballistics. The negative differential pressure isn't generated in the case without the heat transfer of propellants.

Development of Numerical Model for Igniter and Study on Initial Ignition of Interior Ballistics (강내탄도의 점화기 해석 모델 개발 및 초기 점화 연구)

  • Sung, Hyung-Gun;Jang, Jin-Sung;Lee, Sang-Bok;Choi, Dong-Whan;Roh, Tae-Seong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.2
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    • pp.105-113
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    • 2013
  • A numerical model of the igniter for the interior ballistics has been developed by combining lumped parameter model with the theoretical equation of orifice. With the developed model of the igniter, the numerical study on characteristics of the interior ballistics has been conducted according to the igniter configuration in terms of igniter length, side hole diameter, and distribution of side holes. As results of the calculation of the pressure difference between the breech and shot base, the low-cycle oscillations have been influenced by the igniter length, while the high-cycle oscillations have been affected by the side hole diameter and the distribution of side holes.

Modeling and Numerical Investigation of the Biomechanical Interaction for Human-Rifle System

  • Chae, Je-Wook;Lee, Young-Shin
    • Journal of Mechanical Science and Technology
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    • v.18 no.12
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    • pp.2069-2079
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    • 2004
  • This paper represents the description of a complex mathematical model of biomechanical interaction for human-rifle system during shooting. The model is developed by finite element method using bar elements. And three typical shooting positions, i.e. standing, kneeling and prone are used. Characteristics of interior/exterior ballistics and behaviors of human-rifle system are evaluated by this model, which takes into account the influence of environment, bullet, powder, barrel geometry parameters and anthropological parameters. The results of this study can be applied to anthropology, biomechanics, medical science, gait analysis, interior ballistics and exterior ballistics.

Study on Numerical Analysis Method for Moving Boundary of Interior Ballistics (강내탄도의 이동경계면 해석을 위한 수치해석 기법 연구)

  • Kim, In-Joo;Jang, Jin-Sung;Sung, Hyung-Gun;Roh, Tae-Seong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.760-763
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    • 2010
  • The expansion of 1D numerical code to 2D or 3D is needed in order to improve the analysis accuracy of the interior ballistics. The cut cell method has been imposed for the code expansion to multi dimensions. The MUSCL-Hancock scheme as a high resolution method has been selected. A feasibility of the cut cell method has been verified by analyzing the free piston problem.

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Development of Code for Numerical Analysis of Interior Ballistics using Eulerian-Lagrangian Approach and SMART scheme (Eulerian-Lagrangian 접근법과 SMART scheme을 이용한 강내탄도 전산해석 코드 개발)

  • Sung, Hyung-Gun;Jang, Jin-Sung;Lee, Sang-Bok;Choi, Dong-Whan;Roh, Tae-Seong;Jang, Young-Jae
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.3
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    • pp.349-357
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    • 2010
  • In this paper, a numerical code for the interior ballistics has been investigated. The Eulerian-Lagrangian approach and the SMART scheme have been used in the numerical code for the grain combustion. The translational kinetic energy of the projectile and work done against barrel friction have been considered only. The ghost cell extrapolation method has been used for the chamber change with the projectile movement. The calculation results of the numerical code have been compared and verified through those of IBHVG2 code.

Comparative Study of Propellant Modeling in Chamber of Interior Ballistic (강내탄도의 약실 내 추진제 모델링 비교연구)

  • Jang, Jin-Sung;Sung, Hyung-Gun;Roh, Tae-Seong;Choi, Dong-Whan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.668-671
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    • 2010
  • Comparative study on propellant modeling has been investigated using a non-dimensional method and an one-dimensional method. The propellant location in the chamber can not be described by the non-dimensional method. It is, however, possible for the one-dimensional method to describe. Therefore, the analysis of the interior ballistics according to the propellant arrangements has been performed by the one-dimensional method. The negative differential pressure in the chamber could be predicted and the necessity of the one-dimensional modeling for the analysis of the interior ballistics has been confirmed.

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Study on the Propellant Position for the Decrease of the Differential Pressure in the Interior Ballistics of a Gun Propulsion System (강내탄도 내 차압 감소를 위한 추진제 위치 연구)

  • Jang, Jin-Sung;Sung, Hyung-Gun;Roh, Tae-Seong;Choi, Dong-Whan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.1
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    • pp.72-78
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    • 2012
  • The position effect of the solid propellant in the combustion chamber on the decrease of the differential pressure has been investigated using the IBcode. Generally the metallic cartridge or CCC (combustible cartridge case) are used to load the propellant of the gun propulsion system. The position of the cartridge(propellant) is, therefore, a major factor for the interior ballistics in case the combustion chamber is larger than the cartridge. In this study, three different positions in the empty space of the chamber have been considered. As results, the case of the propellant located in the region near the base and breech has shown that the negative differential pressure and the difference between the breech pressure and the base pressure are much higher than those of the case of the propellant located in the center of the chamber. The case of the propellant in the center of the chamber is, therefore, more profitable to improve the performance of the interior ballistics.

Study on the Propellant Position for the Decrease of the Differential Pressure of the Interior Ballistics (강내탄도 내 차압 감소를 위한 추진제 위치 연구)

  • Jang, Jin-Sung;Sung, Hyung-Gun;Roh, Tae-Seong;Choi, Dong-Whan
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.236-241
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    • 2011
  • The position effect of the solid propellant in the combustion chamber on the decrease of the differential pressure has been investigated using the IBcode. Generally the metallic cartridge or CCC (combustible cartridge case) as the propellant for the cannon has been loaded. The position of the propellant(cartridge) is, therefore, a major factor for the interior ballistics in case the combustion chamber is larger than the cartridge. In this study, three cases of the existence of empty space in the chamber has been considered. As results, the case of the propellant located in the region near the base and breech has shown that the negative differential pressure and the difference between the breech pressure and the base pressure are much higher than those of the case of the propellant located in the center of the chamber. The case of the propellant in the center of the chamber is, therefore, more profitable to improve the performance of the interior ballistics.

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Performance Analysis of Interior Ballistics using 1-D Numerical Method (1차원 수치 해석을 통한 강내탄도 성능해석)

  • Jang, Jin-Sung;Sung, Hyung-Gun;Roh, Tae-Seong;Choi, Dong-Whan
    • Journal of the Korea Institute of Military Science and Technology
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    • v.15 no.3
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    • pp.241-249
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    • 2012
  • Performance analysis of the interior ballistics has been conducted using the 1-D numerical code called IBcode according to the various conditions such as length of ignition-gas injector, amount of ignition-gas, mass of projectile, and drag force of projectile. In case of the length of ignition-gas injector, the 25~100 % of the full-injector length has been considered as well as the mass & mass flow of the ignition-gas. The mass of the projectile 5~70 kg and its drag force of 0~69 MPa have been also considered. Variables such as breech & base pressure, negative differential pressure and muzzle velocity for the performance analysis have been sorted, too. Firing conditions for the optimal performance have been investigated through these variables.