• Title/Summary/Keyword: Exterior Ballistics

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The Effect of Changes in Atmospheric Pressure, Temperature and Humidity on the Exterior Ballistics of a Small Rifle (압력, 온도 및 습도의 변화가 소총탄도에 미치는 영향)

  • ;;Lee, Hung Joo;Kwak,Youn Kean
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.3 no.1
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    • pp.10-17
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    • 1979
  • The exterior ballistics of small rifles mist be analyzed for the shooter and coach who are seriously interested in attainment of maximum performance in the art of rifle marksmanship. It provides also a basic reference material for the designers of rifles having better hitting rates. The exterior ballistics are computed using a state vector analysis and presented to facilitate use by individuals according to the atmospheric conditions. The ballistics are changed by the pressure, temperature and humidity of the air.

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.

The Vertical Deviation of the Impact Point from and Aiming Point at an Inclined shooting Ranges (소총의 상하향 사격시 탄도학상의 수직편차)

  • ;;Chang, Won Hong
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.2 no.2
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    • pp.47-51
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    • 1978
  • In order to improve the hitting rate in the shot of rifles, it is required that the analysis of exterior ballistics and the line of sight. One of the important factors influenced a marksman using a rifle obtained the zero-setting of a rifle at the horizontal range, is the deviation of the impact point from the aiming point when the shooting is performed in an inclined ranges. The deviation usually cccurs from the reaction force along the bore line, the characteristics of exterior ballistics, and the error of a shooting range judgement by the inclined range. This study is concerned with the problem of the vertical difference between the impact and aiming point in the inclined shooting ranges. The computing method to find the vertical difference is represented. This method is applied for and experimental rifle in three cases, (1) hofizontal shooting ranges, (2) upper inclined shooting ranges, and (3) lower inclined shooting ranges.

Fire Power Analysis for Concept Exploration of Combat Vehicle (전투차량체계의 개념탐색을 위한 화력성능분석)

  • Lim, O-Kaung;Choi, Eun-Ho;Ryoo, Jae-Bong
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.22 no.3
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    • pp.251-258
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    • 2009
  • At the stage conceptual design, combat vehicle is classified into three general categories of fire power, mobility and physical properties of system. The present research is restricted to fire power and its optimization. At the stage of conceptual designing of system, it is appropriate to consider major variables affecting fire power - including the weight of bullet, which exerts a direct influence on destroying effect, maximum range which takes long range firing in consideration. To estimate the maximum firing range, a simple interior ballistic and an exterior ballistic model were built by using the lumped parameter method, Le Duc method and point mass trajectory model. Design of experiment and regression analysis was used to derive simulations of fire power. Finally, response surface models were built and design variables were analyzed.

Preliminary Design and Analysis of the Small-scale Hybrid Rocket Motor (소형 하이브리드 로켓 모터 기초 설계 및 해석)

  • Kim, Sun-Kyoung;Cho, Min-Kyung;Yoon, Chang-Jin;Kim, Jin-Kon;Sung, Hong-Gye;Moon, Hee-Jang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.415-418
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    • 2006
  • 하이브리드 추진제는 연소 중 연료의 후퇴율 및 연소 면적의 변화로 인해 O/F비가 변화하므로 이로 인해 설계 및 해석에 어려움을 가지게 된다. 본 연구에서는 요구임무를 만족하는 하이브리드 로켓모터에 대한 설계를 수행하였다. 하이브리드 모터의 기초 설계를 실시하고 그 결과를 이용하여, 일정한 산화제 유량이 공급된다는 가정 하에, 연소 시 연소면적변화에 따른 O/F비 변화를 고려한 하이브리드 모터의 내탄도 해석을 실시하였으며, 그 결과를 이용하여 로켓의 외탄도 해석을 실시하였다.

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Launch and Altitude Measurement of Small Hybrid Rocket (소형 하이브리드 로켓의 시험 발사 및 고도 측정)

  • Oh, Ji-Sung;Shin, Jun-Su;Moon, Keun-Hwan;Lee, Jung-Pyo;Moon, Hee-Jang;Sung, Hong-Gye;Kim, Jin-Kon
    • Journal of Aerospace System Engineering
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    • v.4 no.3
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    • pp.29-33
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    • 2010
  • In this study, small hybrid rocket was launched and flight altitude was measured. Flight path of rocket was analyzed with exterior ballistics analysis result. The data acquisition equipment was loaded in rocket and two launch test were performed. HDPE was used as fuel and N20 as oxidizer for this study.

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Flow Visualization and Unstructured Grid Computation of Flow over a High-Speed Projectile (고속탄자 유동의 가시화 실험 및 비정렬격자 계산)

  • 이상길;최서원;강준구;임홍규;백영호;김두연;강호철
    • Transactions of the Korean Society of Automotive Engineers
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    • v.6 no.2
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    • pp.12-20
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    • 1998
  • Exter ballistics of a typical high-speed projectile is studied through a flow-visualization experiment and an unstructured grid Navier-Srokes computation. Experiment produced a schlieren photograph that adequately shows the characteristic features of this complex flow, namely two kinds of oblique cone shocks and turbulent wake developing into the downstream. A hybrid scheme of finite volume-element method is used to simulate the compressible Reynolds-Averaged Navier-Stok- es solution on unstructured grids. Osher's approximate Riemann solver is used to discretize the cinvection term. Higher-order spatial accuracy is obtained by MUSCL extension and van Albada ty- pe flux limiter is used to stabilize the numerical oscillation near the solution discontinuity. Accurate Gakerkin method is used to discretize the viscous term. Explict fourth-order Runge-Kutta method is used for the time-stepping, which simplifies the application of MUSCL extension. A two-layer k-$\varepsilon$ turbulence model is used to simulate the turbulent wakes accurately. Axisymmetric folw and two-dimensional flow with an angle of attack have been computed. Grid-dependency is also checked by carrying out the computation with doubled meshes. 2-D calculation shows that effect of angle of attack on the flow field is negligible. Axi-symmetric results of the computation agrees well with the flow visualization. Primary oblique shock is represented within 2-3 meshes in numerical results, and the varicose mode of the vortex shedding is clearly captured in the turbulent wake region.

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