• Title/Summary/Keyword: ballistic limit

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An upper bound analysis for the plugging type of ballistic perforation on the double and multi-layered armour plates (복층 및 다층장갑판재의 관통에 대한 상부경계이론 해석)

  • 이종우
    • Journal of the Korea Institute of Military Science and Technology
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    • v.3 no.2
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    • pp.35-41
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    • 2000
  • A modified theoretical analysis of the ballistic perforation on the double and multi-layered armour plates using an upper bound method has been presented in this paper. A modified model based on the suggestion of the Awerbuch-bodner model has been adapted and extended into double and multi-layered armour plates when the plugging type of penetration has been occurred. The residual projectile speed, ballistic limit velocity and contact time during the penetration process have been derived from the equation of motion at each stage.

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Effect of rebar spacing on the behavior of concrete slabs under projectile impact

  • Abbas, Husain;Siddiqui, Nadeem A.;Almusallam, Tarek H.;Abadel, Aref A.;Elsanadedy, Hussein;Al-Salloum, Yousef A.
    • Structural Engineering and Mechanics
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    • v.77 no.3
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    • pp.329-342
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    • 2021
  • In this paper, the effect of different steel bar configurations on the quasi-static punching and impact response of concrete slabs was studied. A total of forty RC square slab specimens were cast in two groups of concrete strengths of 40 and 63 MPa. In each group of twenty specimens, ten specimens were reinforced at the back face (singly reinforced), and the remaining specimens were reinforced on both faces of the slab (doubly reinforced). Two rebar spacing of 25 and 100 mm, with constant reinforcement ratio and effective depth, were used in both singly and doubly reinforced slab specimens. The specimens were tested against the normal impact of cylindrical projectiles of hemispherical nose shape. Slabs were also quasi-statically tested in punching using the same projectile, which was employed for the impact testing. The experimental response illustrates that 25 mm spaced rebars are effective in (i) decreasing the local damage and overall penetration depth, (ii) increasing the absorption of impact energy, and (iii) enhancing the ballistic limit of RC slabs. The ballistic limit was predicted using the quasi-static punching test results of slab specimens showing a strong correlation between the dynamic perforation energy and the energy required for quasi-static perforation of slabs.

Device modelling and performance analysis of two-dimensional AlSi3 ballistic nanotransistor

  • Chuan, M.W.;Wong, K.L.;Hamzah, A.;Rusli, S.;Alias, N.E.;Lim, C.S.;Tan, M.L.P.
    • Advances in nano research
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    • v.10 no.1
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    • pp.91-99
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    • 2021
  • Silicene is an emerging two-dimensional (2D) semiconductor material which has been envisaged to be compatible with conventional silicon technology. This paper presents a theoretical study of uniformly doped silicene with aluminium (AlSi3) Field-Effect Transistor (FET) along with the benchmark of device performance metrics with other 2D materials. The simulations are carried out by employing nearest neighbour tight-binding approach and top-of-the-barrier ballistic nanotransistor model. Further investigations on the effects of the operating temperature and oxide thickness to the device performance metrics of AlSi3 FET are also discussed. The simulation results demonstrate that the proposed AlSi3 FET can achieve on-to-off current ratio up to the order of seven and subthreshold swing of 67.6 mV/dec within the ballistic performance limit at room temperature. The simulation results of AlSi3 FET are benchmarked with FETs based on other competitive 2D materials such as silicene, graphene, phosphorene and molybdenum disulphide.

A new method to estimate the striking velocity for small caliber projectiles (소구경 탄자의 충돌속도 추정방법 제안)

  • Yoo, Sangjun;Kim, Jeyong
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.15 no.3
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    • pp.1288-1293
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    • 2014
  • This paper proposes a new method to estimate the striking velocity for ballistic limit velocity in MIL-STD-662F. The method from MIL-STD-662F needs relative air density, drag coefficient, form factor, ballistic coefficient for estimating striking velocity. So precedent studies are essential. However, the new method can estimate striking velocity only using measured velocities and distance between the screen and the target. To prove new method, we compared estimation of striking velocity from both the new method and the method from MIL-STD-662F on the basis of datain PRODAS. The new method shows bigger errors in some velocity ranges. But it could still calculate ballistic limit velocity. It also shows smaller errors in most velocity ranges.

Numerical Simulation of High Velocity Impact of Circular Composite Laminates

  • Woo, Kyeongsik;Kim, In-Gul;Kim, Jong Heon;Cairns, Douglas S.
    • International Journal of Aeronautical and Space Sciences
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    • v.18 no.2
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    • pp.236-244
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    • 2017
  • In this study, the high-velocity impact penetration behavior of $[45/0/-45/90]_{ns}$ carbon/epoxy composite laminates was studied. The considered configuration includes a spherical steel ball impacting clamped circular laminates with various thicknesses and diameters. First, the impact experiment was performed to measure residual velocity and extent of damage. Next, the impact experiment was numerically simulated through finite element analysis using LS-dyna. Three-dimensional solid elements were used to model each ply of the laminates discretely, and progressive material failure was modeled using MAT162. The result indicated that the finite element simulation yielded residual velocities and damage modes well-matched with those obtained from the experiment. It was found that fiber damage was localized near the impactor penetration path, while matrix and delamination damage were much more spread out with the damage mode showing a dependency on the orientation angles and ply locations. The ballistic-limit velocities obtained by fitting the residual velocities increased almost linearly versus the laminate diameter, but the amount of increase was small, showing that the impact energy was absorbed mostly by the localized impact damage and that the influence of the laminate size was not significant at high-velocity impact.

A Study on the Macroscopic Combustion Models of Gun Propellants (화포추진제의 거시적 연소모델에 대한 연구)

  • 윤재건;현형수
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.8
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    • pp.2201-2209
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    • 1994
  • Macroscopic combustion models used in gun interior ballistic codes are discussed and experimental methods to measure propellant burning rate are reviewed. Comparing with gun firing results, the limit of combustion model is shown and modified combustion model is proposed. But combustion model should be selected with respect to total gun system including propellants.

Design Study of a Small Scale Soft Recovery System

  • Yoo, Il-Yong;Lee, Seung-Soo;Cho, Chong-Du
    • Journal of Mechanical Science and Technology
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    • v.20 no.11
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    • pp.1961-1971
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    • 2006
  • A soft recovery system (SRS) is a device that stops a high speed projectile without damaging the projectile. The SRS is necessary to verify the shock resistant requirements of microelectronics and electro-optic sensors in smart munitions, where the projectiles experience over 20,000 g acceleration inside the barrel. In this study, a computer code for the performance evaluation of a SRS based on ballistic compression decelerator concept has been developed. It consists of a time accurate compressible one-dimensional Euler code with use of deforming grid and a projectile motion analysis code. The Euler code employs Roe's approximate Riemann solver with a total variation diminishing (TVD) method. A fully implicit dual time stepping method is used to advance the solution in time. In addition, the geometric conservation law (GCL) is applied to predict the solutions accurately on the deforming mesh. The equation of motion for the projectile is solved with the four-stage Runge-Kutta time integration method. A small scale SRS to catch a 20 mm bullet fired at 500 m/s within 1,600 g-limit has been designed with the proposed method.

A Study on the Damage Design of Military Aircraft Structure Material by Armor Piercing Bullet Hit (철갑탄 피격에 의한 군용 항공기 구조재료의 손상설계에 관한 연구)

  • Hur, Jang-Wook;Hyun, Young-Jin
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.6
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    • pp.1051-1057
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    • 2010
  • Database for the damage reference by armor piercing bullet test was established for both tube and plate specimens having a range of thickness. As the inclined angles of hit are increasing, it has been found that penetration damage diameter tends to increases accordingly in both specimen of the tube and plate, and such penetration damage diameter on the rear side becomes bigger than those on the front side. The tube specimen showed that the damage becomes bigger when central areas rather than the peripheral were hit. Through the plate test, it also has been found that the penetration ballistic limit for Al alloy is about 25.4mm and that of stainless steel about 12.7mm. From the fatigue analysis results using the database for damage reference, it has been identified whether the safety requirements of military aircraft could be met.

The experimental investigation for penetration depth and shape of aluminum alloy plates by 5.56mm ball projectile with striking velocities between 350 and 750㎧ (고속충격시 볼탄에 의한 알루미늄 합금의 관통 깊이와 형상에 관한 실험적 연구)

  • 손세원;김희재;김영태
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2002.10a
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    • pp.800-803
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    • 2002
  • This investigation describes and analyses the experimental results proper to the penetration of Al5052-H34 alloy plates of thickness 6, 12 and 16mm(T/D=1, 2, 3) by 5.56mm ball projectiles over the velocity range 350-750㎧. All the high velocity impact tests were carried out at normal impact angle, i.e. zero obliquity. The experimental results presented the variation of depth of penetration, bulge height and diameter, plugged length and diameter with the velocity fur tests on each plate of a given thickness in order to determine the deformation shapes of 5.56mm ball projectiles and targets. Also the protection ballistic limit($V_50$) tests were conducted.

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방탄재료의 경방탄 특성에 관한 연구

  • 손세원;유명재
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.94-94
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    • 2004
  • 고성능 섬유강화 복합재료는 단위 중량당 강성과 강도가 높으면서 가격도 저렴하여 여러 산업분야에서 널리 사용되고 있으며 특히, 경량임에도 충격에 대한 저항성이 우수하여 방탄재료로의 군사적, 민간용 이용도가 날로 증가되고 있다. 그러나 고속 충격 탄자와 같이 관통성이 뛰어난 위협 조건으로부터의 방호를 목적으로 장갑을 설계할 매는 단일 재료만으로는 충분한 방탄 성능을 가질 수 없는 경우가 많다. 이런 경우는 충격 전면에서 충격 탄자의 탄두를 일차적으로 무디게 하거나 파쇄시켜 탄자의 형상을 변화시키고, 변형된 탄자의 계속적인 관통에 대한 저항능력이 우수한 재료를 사용하여 두가지 성질을 동시에 만족시키는 장갑재료의 개발이 요구되고 꾸준히 연구되어 왔다.(중략)

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