• International Journal of Aeronautical and Space Sciences
• /
• 제16권2호
• /
• pp.190-205
• /
• 2015

In this paper, the impact damage behavior of USN-150B carbon/epoxy composite laminates subjected to high velocity impact was studied experimentally and numerically. Square composite laminates stacked with $[45/0/-45/90]_{ns}$ quasi-symmetric and $[0/90]_{ns}$ cross-ply stacking sequences and a conical shape projectile with steel core, copper skin and lead filler were considered. First high-velocity impact tests were conducted under various test conditions. Three tests were repeated under the same impact condition. Projectile velocity before and after penetration were measured by infrared ray sensors and magnetic sensors. High-speed camera shots and C-Scan images were also taken to measure the projectile velocities and to obtain the information on the damage shapes of the projectile and the laminate specimens. Next, the numerical simulation was performed using explicit finite element code LS-DYNA. Both the projectile and the composite laminate were modeled using three-dimensional solid elements. Residual velocity history of the impact projectile and the failure shape and extents of the laminates were predicted and systematically examined. The results of this study can provide the understanding on the penetration process of laminated composites during ballistic impact, as well as the damage amount and modes. These were thought to be utilized to predict the decrease of mechanical properties and also to help mitigate impact damage of composite structures.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2002년도 춘계학술대회 논문집
• /
• pp.865-868
• /
• 2002

This study investigated the shape deformation of ball projectile(5.56mn) under the low energy impact by the use of the drop weight impact tester. ball projectile(5.56mm) consisted of the copper face with a lead core. The impact conditions were changed with the variations of the mass and the drop height of the impact tup. Shape deformation of ball projectile(5.56mm) after low velocity impact was measured using a video microscope and CCD camera. The test result showed that impact energy by changing of drop height of the impact tup affected shape deformation of ball projectile(5.56mm). So, it is important to study the relativity between shape deformation of ball projectile(5.56mm) and ballistic protection of plate(such as hybrid composite laminates) under the high velocity impact.

• Composites Research
• /
• 제26권3호
• /
• pp.175-181
• /
• 2013

고속충격을 받는 복합재 적층판의 충격거동 특성 중에서 관통 후 잔류속도, 시편에 의한 충격흡수에너지 그리고 충격손상영역에 대한 평가와 예측이 중요하다. 본 논문에서는 고속충격을 받는 Carbon/Epoxy 복합재 적층판의 잔류속도와 흡수에너지를 준실험적 방법을 통하여 예측할 수 있는 방법을 제안하였다. 고속충격에 의한 시편의 흡수에너지를 정적에너지와 동적에너지로 구분하였으며 정적에너지는 보강섬유의 파손과 정적 탄성에너지와 관련 있는 준정적압입실험을 통한 관통에너지를 사용하였다. 동적에너지는 고속충격 시 시편 일부의 움직임과 관련한 운동에너지에 대하여 몇 가지 모델을 제안하여 비교하였다. 공압을 이용한 고속충격실험을 수행하고 예측 값과 비교 분석하였다. 시편의 손상영역은 C-scan을 통하여 측정하였다. 관통한계속도보다 큰 초기 속도인 경우, 정적에너지인 관통에너지 뿐 만 아니라 시편의 동적 에너지가 시편 전체 흡수에너지에 크게 기여함을 알 수 있었다.

• 한국시뮬레이션학회논문지
• /
• 제29권1호
• /
• pp.1-9
• /
• 2020

과학기술의 발전에 따라 탄도탄에 대한 위협이 나날이 증대되고 있으며, 이러한 위협에 대처하기 위한 탄도탄 요격미사일에 대한 개발이 요구되고 있다. 대탄도탄용 요격미사일의 개발을 위해서는 요격시험이 필수적이다. 시험을 통해 얻은 계측자료를 활용하여 요격미사일을 포함한 전체적인 요격 시스템의 성능을 확인할 수 있다. 그러나 요격시험 시에는 요격에 의한 파편이 발생되기 때문에 안전을 위한 민간인의 접근 통제가 필요하다. 따라서 요격시험에 앞서 요격 파편에 대한 안전구역의 신뢰도 높은 추정이 선행되어야 한다. 본 논문에서는 모델링 분석 및 시뮬레이션을 활용하여 요격 파편에 대한 안전구역을 산출하였다. 우선, 탄도탄과 요격미사일의 발사단계에서 요격까지의 전 과정에 대한 시뮬레이션을 수행하였고, 요격 시점에서의 상대 속도 및 상대 각도를 산출하였다. 이 결과를 활용하여 요격 시의 에너지를 계산하고 요격 파편의 방출속도를 산출하였다. 이후, 파편에 작용하는 항력과 중력을 고려하여 낙하 궤적을 산출하였고, 파편의 낙하 지점과 위험도를 종합적으로 고려하여 최종 안전구역을 산출하였다.

• 품질경영학회지
• /
• 제47권2호
• /
• pp.283-294
• /
• 2019

Purpose: Although the development of bulletproof helmets continues to be carried out, little has been improved in testing methods. Therefore, in this study, we studied the improvement of the test method of the domestic bulletproof helmet. Methods: The causes of head damage in the battlefield and the trends of bulletproof helmet development in developed countries were analyzed. In addition, improvements were derived by comparing the test methods of bulletproof helmet in Korea and the United States. Results: The results of the improvement by comparing the test methods of bulletproof helmet in Korea and the United States are as follows First, it is an addition to the scope of environmental treatment. Second, it is an addition to the level of protection. Third, the addition of the level of protection by impact. Conclusion: This study considered testing methods to prevent head injuries to shocks that cannot be identified by conventional methods. In addition, it considered testing methods for various threats by improving protection performance to advanced countries' levels.

• Steel and Composite Structures
• /
• 제22권4호
• /
• pp.777-796
• /
• 2016

In this paper, the behavior of woven E-glass fabric composite laminate was experimentally investigated under quasi-static indentation and high velocity impact by flat-ended, hemispherical, conical (cone angle of $37^{\circ}$ and $90^{\circ}$) and ogival (CRH of 1.5 and 2.5) cylindrical perforators. Moreover, the results are compared in order to explore the possibility of extending quasi-static indentation test results to high velocity impact test results in different characteristics such as perforation mechanisms, performance of perforators, energy absorption, friction force, etc. The effects of perforator nose shape, nose length and nose-shank connection shapes were investigated. The results showed that the quasi-static indentation test has a great ability to predict the high velocity impact behavior of the composite laminates especially in several characteristics such as perforation mechanisms, perforator performance. In both experiments, the highest performance occurs for 2.5 CRH projectile and the lowest is related to blunt projectiles. The results show that sharp perforators indicate lower values of dynamic enhancement factor and the flat-ended perforator represents the maximum dynamic enhancement factor among other perforators. Moreover, damage propagation far more occurred in high velocity impact tests then quasi-static tests. The highest damage area is mostly observed in ballistic limit of each projectile which projectile deviation strongly increases this area.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2000년도 제15회 학술강연회논문초록집
• /
• pp.29-29
• /
• 2000

추진제의 폭연 특성을 실험실 규모로 측정하는 시험방법으로 NAWC에서 개발한 BIC (Ballistic Impact Chamber) 시험과 SNPE에서 개발한 Shotgun/RQ Bomb 시험이 있다. SNPE에서는 화약과 추진제가 UNO 위험등급 분류체계에서 1.6급수(우연한 개시나 반응의 전환 가능성이 거의 없는 매우 둔감한 물질)로 분류되는 기준을 UN Test Series 7c(ii)에 탄속 150m/s에서 dP/dt가 15MPa 이내로 규정하고 있다.(중략)

• 한국추진공학회지
• /
• 제6권1호
• /
• pp.30-38
• /
• 2002

복합재 연소관에 기계적 물성을 향상시킨 추진제를 충전한 모타와 복합재 연소관에 기존의 내탄도 성능을 어느 정도 유지하며 연소속도의 조절로 추진제의 둔감화를 시도한 추진제를 충전한 로켓모타에 대하여 탄환충격시험을 실시하여 그 반응을 비교·분석하였다.

• International Journal of Aeronautical and Space Sciences
• /
• 제13권3호
• /
• pp.282-295
• /
• 2012

Fiber reinforced polymer matrix composites are widely used to provide protection against ballistic impact and blast events. There are several factors that govern the structural response and mechanical properties of a textile composite structure, of which the fiber-matrix interfacial behavior is a crucial determinant. This paper reviews the microbond or microdroplet test methodology that is used to characterize the fiber-matrix interfacial behavior, particularly the interface shear strength (IFSS). The various analytical, experimental, and numerical approaches applied to the microbond test are reviewed in detail.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2001년도 춘계학술대회논문집A
• /
• pp.561-566
• /
• 2001

A long bar impact test to alumina plates(AD 85 and AD 90) was carried out by using fabricated impact testing apparatus. The apparatus adopting a long bar of 2.1m in length made it possible to measure directly the applied impact force to the specimen during bar impact. The dimension of specimens was $33{\times}33mm$ and thickness was 3.4mm. Confinement of D2=18mm outer diameter and D1=10.5mm inner diameter was used to provide contact pressure to the specimen. Contact pressure of p=100 or 200MPa was applied to specimen before impact test. Damage caused in those cases were compared with the case of without contact pressure. The damage of specimen was different depending upon the pressure level of confinement. The existence of confinement had suppressed the development of radial cracks from the bottom of specimen and reduced the extent of damage as compared with cases without contact pressure(p=0MPa). Because the application of contact pressure to the specimen increased the apparent flexural stiffness of specimen during bar impact, it had produced the change of developed damage in the specimen; from the radial cracks to the local contact stress dominant damage. It would contribute to the improvement of the ballistic property in ceramic plates.