• 제목/요약/키워드: missile penetration

검색결과 21건 처리시간 0.019초

Safety assessment of an underground tunnel subjected to missile impact using numerical simulations

  • Thai, Duc-Kien;Nguyen, Duy-Liem;Pham, Thanh-Tung;Pham, Thai-Hoan
    • Computers and Concrete
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    • 제27권1호
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    • pp.1-12
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    • 2021
  • This work presents a safety assessment of an underground tunnel subjected to a ballistic missile attack employing the numerical approach. For the impact simulation, a box shaped reinforced concrete (RC) structure with a cross section dimension of 8.0×10.0 m under a soil layer that was attacked by a SCUD missile was modeled using finite element (FE) software LS-DYNA. SCUD missile is one of a series of tactical ballistic missiles developed by Soviet Union during the Cold War, which is adopted for a short-range ballistic missile. The developed FE simulation for the penetration depth of the missile impacting into the soil structure was verified from the well-known formula of the penetration prediction. The soil-structure interaction, the soil type, and the impact missile velocity effects on the penetration depth of the missile into the different soil types were investigated. The safety assessment of the underground tunnel was performed with regard to the different depths of the underground tunnel. For each missile velocity and soil type, a specific depth called the unsafe depth was obtained from the analysis results. The structure beneath the soil beyond this depth remains safe. The unsafe depth was found to be increased with the increasing missile velocity.

Mechanics of missile penetration into geo-materials

  • Siddiqui, N.A.;Abbas, H.
    • Structural Engineering and Mechanics
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    • 제13권6호
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    • pp.639-652
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    • 2002
  • The present study aims to improve an existing model for the prediction of deceleration time history, penetration depth and forces on ogive and conical nose shaped missiles under normal impact into geo-material targets. The actual ogive nose shaped missile has been considered in the analysis and the results thus obtained have been compared with the existing model and significant improvements are found. A close proximity in the results has also been observed with the experimental values. The results of ogive nose shaped missile have also been compared with equivalent conical nose shaped missile. Variation of radial stresses along nose length and radial direction has been studied. Effect of CRH on missile penetrating performance has been investigated.

Reliability of underground concrete barriers against normal missile impact

  • Siddiqui, N.A.;Khan, F.H.;Umar, A.
    • Computers and Concrete
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    • 제6권1호
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    • pp.79-93
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    • 2009
  • In the present paper, a methodology has been presented for the reliability assessment of concrete barriers that lie at a certain depth in the soil, and a missile (a rigid projectile) impacts the top of the soil cover normally, and subsequently after penetrating the soil cover completely it hits the barrier with certain striking velocity. For this purpose, using expressions available in the literature, striking velocity of missile at any depth of soil has been derived and then expressions for the depths of penetration in crater and tunnel region of concrete barrier have been deduced. These depths of penetration have been employed for the derivation of limit state functions. Using the derived limit state functions reliability assessment of underground concrete barrier has then been carried out through First Order Reliability Method (FORM). To study the influence of various random variables on barrier reliability, sensitivity analysis has also been carried out. In addition, a number of parametric studies is conducted to obtain the results of practical interest.

대전차유도무기의 종말 받음각 및 입사각의 상관관계에 의한 표적 파괴율 분석 (Kill Probability Analysis Based on the Relation between Final Angle of Attack and Impact Angle of a Guided Anti-tank Missile)

  • 정동길
    • 한국군사과학기술학회지
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    • 제13권4호
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    • pp.520-527
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    • 2010
  • The kill probability of a missile depends on guidance error, warhead performance, and etc. In this paper, we analyzed the kill probability of anti-tank missile in a new approach. Under the condition that the missile hit the target, we studied the effect of angle of attack and impact angle. High impact angle increase the probability that the missile hits the upper armour which is relatively weaker, while high angle of attack at the impact instant decreases the effectiveness of the jet induced by the warhead. We proposed a way to increase the capability of penetration by analyzing the interrelation between impact angle and angle of attack.

철도차량 ROOF 구조의 시험 사례 고찰 (The Review of Test cases on the Roof Structure of Railway Vehicles)

  • 김재웅;박영훈;김정남
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2006년도 추계학술대회 논문집
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    • pp.219-224
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    • 2006
  • In this paper, to verify the safety of railway vehicle structure, we describe the test methods of roof structure. The purpose of GM/RT 2100' missile protection article is to minimise the risk of injury which could result from the penetration into a vehicle body by missile such as stones and bricks. we carried out weight drop test on the roof structure in accordance with GM/RT 2100. The test results showed that the penetration did not occer.

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A simplified procedure to incorporate soil non-linearity in missile penetration problems

  • Siddiqui, N.A.;Kumar, S.;Khan, M.A.;Abbas, H.
    • Structural Engineering and Mechanics
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    • 제23권3호
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    • pp.249-262
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    • 2006
  • In this paper, a simplified mathematical procedure is presented to incorporate nonlinearity in soil material to predict the deceleration time history, penetration depth and other relevant parameters for normal impact of missiles into soil targets. Numerical method is employed for these predictions. The results of the study are compared with experimental observations and predictions available in the literature. A good agreement is found with experimental observations and an improvement is observed with existing predictions. A comparison is also made with linear soil model. Some parametric studies are also carried out to obtain the results of practical interest.

대용량 해석을 지원하는 무기체계 연구 개발 전용 모델러 설계 기술 연구 (Study on the Design of CAE Modeler for a Weapon System Supporting a Large Volume CAE Analysis)

  • 송일환;김익준;리경호;유용균;한순흥
    • 한국CDE학회논문집
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    • 제15권1호
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    • pp.43-50
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    • 2010
  • Generation of over one hundred million mesh is essential for getting an exact analysis result of penetration, combustion, and explosion of missile. But because no domestic modeler to support this exists and a modeler only for missile also has not been developed yet, it is too difficult to get this goal. In this research we develop a modeler only for an engineering analysis of missile using 64bit computing system to solve current problems.

유도탄 탄두의 전방구조물 완충효과 연구 (Study on Shock Absorb Effect in front Section of Missile Warhead)

  • 염기선
    • 한국군사과학기술학회지
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    • 제7권2호
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    • pp.118-125
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    • 2004
  • In anti-ship missile, the seeker and guidance control units are located in front of warhead. When the missile hits target, these structures play an important role to warhead structure like a shock absorber Because the shock waves are attenuated, the survival probability of warhead increases which guarantees the explosive train. In this thesis the role of frontal sections is studies. The theoretical analysis and numerical analyses using LS-DYNA code are performed. To prove the effect of shock absorber, the penetration test using subscale prototype warhead are executed.

Compaction process in concrete during missile impact: a DEM analysis

  • Shiu, Wenjie;Donze, Frederic-Victor;Daudeville, Laurent
    • Computers and Concrete
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    • 제5권4호
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    • pp.329-342
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    • 2008
  • A local behavior law, which includes elasticity, plasticity and damage, is developed in a three dimensional numerical model for concrete. The model is based on the Discrete Element Method (DEM)and the computational implementation has been carried out in the numerical Code YADE. This model was used to study the response of a concrete slab impacted by a rigid missile, and focuses on the extension of the compacted zone. To do so, the model was first used to simulate compression and hydrostatic tests. Once the local constitutive law parameters of the discrete element model were calibrated, the numerical model simulated the impact of a rigid missile used as a reference case to be compared to an experimental data set. From this reference case, simulations were carried out to show the importance of compaction during an impact and how it expands depending on the different impact conditions. Moreover, the numerical results were compared to empirical predictive formulae for penetration and perforation cases, demonstrating the importance of taking into account the local compaction process in the local interaction law between discrete elements.

비행체의 경로최적화 (Path Optimization for Aircraft)

  • 김세헌;염건
    • 한국경영과학회지
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    • 제8권1호
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    • pp.11-18
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    • 1983
  • This paper shows a new efficient solution method of finding an optimal path for a cruise missile or aircraft to a target which has the maximal survivability and penetration effectiveness against sophisticated defenses and over varied terrain. We first generate a grid structure over the terrain, to construct a network. Since our network usually has about 10,000 nodes, the conventional Dijkstra algorithm takes too much computational time in its searching process for a new permanent node. Our method utilizes the Hashing technique to reduce the computational time of the searching process. Extensive computational results are presented.

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