• Title/Summary/Keyword: Projectile

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Study on Penetration Characteristics of Tungsten Cylindrical Penetrator (텅스텐 원형 관통자의 관통특성에 관한 연구)

  • Jo, Jong Hyun;Lee, Young Shin;Kim, Jae Hoon;Bae, Yong Woon
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.37 no.9
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    • pp.1083-1091
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    • 2013
  • The design of missile require extremely small warheads that must be highly efficient and lethal. The penetration characteristics of each penetrator and the total number of penetrators on the warhead are obvious key factors that influence warhead lethality. The design of the penetrator shape and size are directly related to the space and weight of the warhead. The design of the penetrator L/D was directly related to the space and weight of the warhead. L and D are the length and the diameter of the projectile, respectively. The AUTODYN-3D code was used to study the effect of penetrator penetration. The objective of numerical analysis was to determine the penetration characteristics of penetrator produced by hypervelocity impacts under different initial conditions such as initial velocity, obliquity angle and L/D of penetrator. The residual velocity and residual mass were decreased with increasing initial impact velocity under $L/D{\leq}4$.

Numerical Analysis on Penetration Reduction of a WHA Penetrator by an Impact of Linear Explosively Formed Penetrator(LEFP) (선형폭발성형탄(LEFP) 충격에 의한 WHA 관통자의 관통성능 감소에 관한 수치해석 연구)

  • Joo, Jaehyun;Choi, Joonhong;Koo, ManHoi;Kim, Dongkyu
    • Journal of the Korea Institute of Military Science and Technology
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    • v.20 no.3
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    • pp.384-392
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    • 2017
  • A linear explosively formed penetrator(LEFP) is a modification of the explosively formed penetrator(EFP). An EFP is axisymmetric and has a dish-shaped liner while LEFP has a rectangular-shaped liner with curved cross section. Upon detonating LEFP forms laterally wide projectile like blade, leaving a long penetration hole on the target. On the other hand, a long-rod tungsten heavy alloy(WHA) penetrator is one of the major threats against most of the ground armored vehicles. In this paper, the feasibility of using an LEFP in protecting against a long-rod WHA penetrator by colliding LEFP into the threat was investigated through a set of numerical simulations. In this study, a scale-down WHA penetrator with length to diameter ratio(L/D) of 10.7 and 7.0 mm diameter was used to represent a long-rod WHA penetrator. LS-DYNA and Multi-Material ALE technique were employed for the simulation. For estimation of the protection effect by LEFP, residual penetration depths into RHA by the threat were compared according to various impact locations against the threat.

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.

Aerodynamic Design of a Canard Controlled 2D Course Correction Fuze for Smart Munition (카나드 기반의 지능탄 조종 장치 공력설계)

  • Park, Ji-Hwan;Bae, Ju-Hyeon;Song, Min-Sup;Myong, Rho-Shin;Cho, Tae-Hwan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.3
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    • pp.187-194
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    • 2015
  • Course correction munition is a smart projectile which improves its accuracy by the control mechanism equipped in the fuze section with canard. In this paper, various aerodynamic configurations of the fuze section were analysed by utilizing a semi-empirical method and a CFD method. A final canard configuration showing the least drag was then determined. During the CFD simulation, it was found that the k-${\omega}$ SST turbulence model combined with O-type grid base is suitable for the prediction of the base drag. Finally, the aerodynamic characteristics of the smart munition and the change of drag due to the canard installation were analysed.

Effect of Intentional Draw & Fade Shots on Golf Swing Mechanics (의도적인 드로우 샷과 페이드 샷이 골프 스윙 역학에 미치는 영향에 관한 연구)

  • Sohn, Jee-Hoon;Ryue, Jae-Jin;Lee, Ki-Kwang;Lim, Young-Tae
    • Korean Journal of Applied Biomechanics
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    • v.20 no.2
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    • pp.149-154
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    • 2010
  • Intentional draw and fade shots could be good weapons for lowering golf score. But how to make such shots? To investigate deterministic variables generating different projectile paths of shots in square stance was the purpose of this study. Ten right-handed male collegiate athletes, showing 1.3 of averaged handicap, participated in this study. They were asked to intentionally perform three different shots such as the straight shot(control condition), draw shot, and fade shot. Swing path, pelvis rotation angle, thorax rotation angle and left forearm supination angle were determined for dependent variables on impact event at each trial. For statistical analysis one-way repeated measures ANOVA were used. The results showed that swing path was one of main factor making differences among three kind of shots. Straight shot vs. Draw shot, Straight shot vs. Fade shot and Draw shot vs. Fade shot showed differences on swing path. And left forearm supination angle revealed significant difference between draw shot and fade shot, showing a significant larger angle of draw shot than fade shot. No other significant difference was detected for the other variables. We found that the shot characteristics were influenced primarily by swing path and left forearm supination angle.

Effect of Urethane Modification on the Anti-Bullet Property of Dyneema/vinylester Composites (우레탄 수지 첨가에 의한 다이니마/비닐에스터 복합재료의 방탄효과 향상 연구)

  • Yoon, T.H.;Cha, Y.M.;Yuck, J.I.;Paik, J.G.;Oh, Y.J.;Kim, H.J.
    • Composites Research
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    • v.24 no.6
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    • pp.7-11
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    • 2011
  • Polyurethane oligomers (PUOs) such as UA8297, UP127 and EB8200 were utilized to enhance the anti-bullet property of Dyneema$^{(R)}$/vinylester composites. First, prepregs of PUO and vinylester (XSR10) were prepared via spray coating on Dyneema$^{(R)}$ fabric at 21 % resin content (by volume). In addition, spray coating and film lamination were also carried out with a mixture of XSR10/PUO for selected PUOs. Next, the prepregs were dried at RT for 1-2 h and then at $100^{\circ}C$ for 30 min to remove the solvent and to provide partial cure when necessary. The prepregs were stacked in 24 layers and cured at $120^{\circ}C$ for 5 min under the contact pressure and for additional 25 min at 150 $kg/cm^2$. Finally, the anti-bullet properties of composite samples were evaluated by measuring $V_{50}$ with simulated fragment projectile (SFP, 17 gr). The results showed a 6.5 and 9.0 % increase of $V_{50}$ with UP127 and EB8200, respectively.

A one-dimensional model for impact forces resulting from high mass, low velocity debris

  • Paczkowski, K.;Riggs, H.R.;Naito, C.J.;Lehmann, A.
    • Structural Engineering and Mechanics
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    • v.42 no.6
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    • pp.831-847
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    • 2012
  • Impact from water-borne debris during tsunami and flood events pose a potential threat to structures. Debris impact forces specified by current codes and standards are based on rigid body dynamics, leading to forces that are dependent on total debris mass. However, shipping containers and other debris are unlikely to be rigid compared to the walls, columns and other structures that they impact. The application of a simple one-dimensional model to obtain impact force magnitude and duration, based on acoustic wave propagation in a flexible projectile, is explored. The focus herein is on in-air impact. Based on small-scale experiments, the applicability of the model to predict actual impact forces is investigated. The tests show that the force and duration are reasonably well represented by the simple model, but they also show how actual impact differs from the ideal model. A more detailed three-dimensional finite element model is also developed to understand more clearly the physical phenomena involved in the experimental tests. The tests and the FE results reveal important characteristics of actual impact, knowledge of which can be used to guide larger scale experiments and detailed modeling. The one-dimensional model is extended to consider water-driven debris as well. When fluid is used to propel the 1-D model, an estimate of the 'added mass' effect is possible. In this extended model the debris impact force depends on the wave propagation in the two media, and the conditions under which the fluid increases the impact force are discussed.

Improvement of Muzzle Localization Using Linear Microphone Array (선형마이크로폰 어레이를 이용한 총구 거리 추정 개선 방법)

  • Jung, Seong-Woo;Kim, Yang-Hann
    • The Journal of the Acoustical Society of Korea
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    • v.34 no.1
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    • pp.60-65
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    • 2015
  • In this paper, we used the sound of gunshots recorded by multiple microphones to increase the accuracy of the calculation of the distance between sniper and the microphone array. This method is crucial for achieving military objectives. Gunshots are comprised of the explosion of driving gas from the muzzle and the supersonic shock wave from the flying bullet. The original distance calculation method compares the time difference of arrival and angle of incidence to estimate the sniper's location. The disadvantage of this method is that when the angles of incidence coincide the margin of error increases, to solve this problem we suggest a new method using the characteristic changes of the shock wave with the increase of perpendicular distance between the microphone and the trajectory of the bullet. This theory is verified by experiments.

A prediction of Ring Frame Composite Properties Using Discretization Method (이산화 기법을 이용한 링프레임 복합재의 기계적 물성 예측)

  • Jeon, Yong Un;Kim, Yong Ha;Kim, Pyung Hwa;Kim, Hwi yeop;Park, Jung Sun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.939-941
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    • 2017
  • The use of composites is increasing for lightweight aerospace structures. Among these structures, the ring frame and the parts of the projectile body are mainly made of a fiber reinforced composite material which is less susceptible such as delamination to structural damage. As the use of fiber reinforced composites increases, interest in modeling efficient methods of stiffness and strength is increasing. This paper predict the mechanical strength according to the repeating unit cell(RUC) of the 2-D triaxial braided composites of fiber reinforced composites. Yarn slice definition, incremental approach and stiffness reduction model were used as strength prediction. Finally, the results of strength prediction are verified by comparing with experimental data of 2-D triaxial braided composites specimens.

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Bacterial Meningitis during Continuous Epidural Block (지속적 경막외 차단중 발생한 세균성 뇌막염)

  • Lee, Jung-Koo;Chung, Jung-Gil
    • The Korean Journal of Pain
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    • v.7 no.1
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    • pp.113-115
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    • 1994
  • Bacterial meningitis is a rare complication of epidural block. As epidural abscess, subarachnoid infection associated with epidural catheters are related to the treatment of pain in diabetic patient whose immune responses have been impaired. A 51-year-old male with non-insulin dependent diabetes came to the pain clinic with neuropathic gain on right thigh and amputated stump of right leg. Treatment consisted of continuous epidural block and subcutaneous tunnelling and epidural morphine with bupivacaine was given on an outpatient basis. Two months later, the patient noted a diffuse frontal headache, projectile vomiting and stiffness neck. These symptoms became more aggrevated over the following 24 h and temperature went up to $38.4^{\circ}C$. A diagnostic lumbar puncture revealed CSF total protein of 747 mg/dl, glucose of 43 mg/dl, and $4320\;WBC/mm^3$. Cultures of epidural catheter tip grew hemolytic staphylococcus epidermidis. A chest x-ray and brain CT scan were negative. Antibiotic therapy with penicillin G and chloramphenicol was given for 15 days. Recovery was uneventful.

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