• 대한전기학회:학술대회논문집
• /
• 대한전기학회 1997년도 하계학술대회 논문집 C
• /
• pp.1205-1209
• /
• 1997

When the short fault current is flowed into a fuse, the notch of element is melted, and burnbacked by arc plasma, which caused by the voltage of fuse at both ends. The cutoff ability of fuse is heavily influenced by the degree of burnback. In this paper, we investigated the amount of burnback to the applied voltage di/dt variation, As a result, we confirmed that the amount of burnback is proportional to the variation of the applied voltage.

• 한국군사과학기술학회지
• /
• 제18권6호
• /
• pp.816-821
• /
• 2015

In this paper, an in-flight prediction method of thrust profiles for solid rocket motors is proposed. Actually, it is very difficult to have detailed information about the performance of the rocket motors beforehand because it is quite sensitive to combustion environments. To overcome this problem, we have developed an algorithm for generating in-flight prediction of rocket motor performance in realistic environments via a reference burnback profile and accelerations measured at a short time-interval just after launch. The performance is evaluated through a lot of flight test results.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2004년도 춘계학술대회
• /
• pp.1570-1575
• /
• 2004

In order to evaluate the performance of fire-fighting agents used to protect structures from heat and fire damages, the thermal characteristics of fire-protection foams are experimentally investigated. The current research focuses on the destruction of a fire-fighting foam subjected to heat radiation. A simple repeatable test for fire-protection foams subjected to fire radiation is developed. This test involves foam generation equipment, a fire source for heat generation, repeatable test procedures, and data acquisition techniques. Results of the experimental procedure indicated that each thermocouple within the foam responded in a similar manner and gradually to a temperature of $15^{\circ}C{\sim}20^{\circ}C$. At this point, each trace generally rises to a temperature of approximately $90^{\circ}C$. The temperature gradient in the foam as time passes increases with increased foam expansion ratio. In addition, it is determined that the temperature gradient along the foam for depth decreases with increased foam expansion ratio.

• 한국추진공학회지
• /
• 제21권3호
• /
• pp.61-67
• /
• 2017

본 연구에서는 VOF 기법을 이용하여 3D 그레인 형상의 연소표면적을 계산하는 프로그램을 개발하고 연소표면적 결과를 이용하여 내탄도 성능해석을 수행하였다. 연소표면적 계산 수행 시 격자 크기, 난류화염속도, 단위 계산시간을 기초로 한 매개변수의 의존성을 확인하고, 상용 3D 모델링 소프트웨어를 이용하여 산출한 면적 결과와 비교하였다. 개발 프로그램으로 산출한 연소표면적 결과를 바탕으로 고체로켓모터의 내탄도 해석을 수행하였다. 임의의 추진제 조성으로 화학평형을 계산하고 시간에 따른 연소표면적 및 모터 내부 압력을 예측하였다. 웹(web) 연소 동안 평균 압력은 5.34 MPa 으로 기존 연구 결과와 약 20%의 차이를 보였다.