• 제목/요약/키워드: Shock intensity

검색결과 127건 처리시간 0.031초

폭발형 고섬광 발생장치의 설계 변수에 관한 실험적 연구 (Experimental Study on Design Parameters of Explosive-driven High-intensity Flash Generator)

  • 김경식;안재운;양희원;권미라
    • 대한기계학회논문집B
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    • 제40권5호
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    • pp.283-288
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    • 2016
  • 목표 대상을 치명적이거나 파괴하지 않고 제압할 수 있는 무기를 비살상무기라 하며, 그중 고섬광발생장치는 강한 섬광으로 적의 광학센서를 무력화시키거나 시력을 일시적으로 마비시키는 무기체계이다. 본 연구에서는 고폭화약에 의한 충격파로 인해 발생한 플라즈마를 이용한 폭발형 고섬광발생장치의 형상에 대한 설계 방안을 도출하여 시료를 제작하고 광학센서를 사용한 기초시험을 수행하였다. 또한, 시험결과를 분석하여 설계 변수에 따른 고섬광 효과를 최대화시키는 방안을 도출하고자 한다. 충전가스 종류로 아르곤보다 제논의 경우 2배 가량 광도가 높게 나타났으며, 비활성가스가 광도에 미치는 영향을 알아보기 위한 비교로써 공기보다 제논의 경우 4배 가량 광도가 높게 나타났다. 또한, 화약량이 증가할수록 원주방향으로 전달되는 충격파가 도달할 수 있는 단면적이 증가할수록 광도가 증가함을 알 수 있었으며, 단일기폭보다 이중기폭의 경우 광원이 2배가 되어 광도도 2배됨을 입증하였다.

Weak Shock Theory를 이용한 초음파의 비선형 전파에 의한 온도 상승 (Temperature Rise due to Nonlinear Propagation of Ultrasound using Weak Shock Theory)

  • 최민주;성굉모;이상은;정병하;이무상
    • 대한의용생체공학회:학술대회논문집
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    • 대한의용생체공학회 1998년도 추계학술대회
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    • pp.74-75
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    • 1998
  • The present study employs weak shock theory and bio-heat transfer function to predict the temperature rise due to nonlinear propagation of high amplitude ultrasound. The theory shows that, for the focused ultrasound which is assumed to have an gaussian beam profile and has the focal intensity of $1000W/cm^2$, the temperature rise of liver tissue exposed for 1 second to the energy lost during nonlinear propagation goes up to about $30^{\circ}C$. This indicate that it is necessary to consider the nonlinear propagation induced heating enhancement when setting exposure condition of high intensity focused ultrasound used for cancer thermotherapy.

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UNSTEADY SUPERSONIC INLET DIFFUSER FLOWS WITH SINUSOIDAL PRESSURE OSCILLATIONS

  • Jong Yun Oh
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 1996년도 제7회 학술강연회논문집
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    • pp.107-116
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    • 1996
  • Numerical simulations have been conducted to characterize unsteady flow structures in an axisymmetric supersonic inlet diffuser with sinusoidal pressure oscillations at the diffuser exit. The formulation is based on the unsteady Navier-Stokes equations and turbulence closure is achieved using a two-layer model with a too-Reynolds-number scheme for the near-wall treatment. The governing equations are formulated in an integral form, and are discretized by the four-stage Runge-Kutta scheme for temporal terms and the Harten-Yee upwind TVD scheme for convective terms. Results indicated that the inlet shock characteristics are significantly modified by acoustic oscillations originating from the combustor. The characteristics of shock/boundarv-layer interactions (such as the size of separation bubble, terminal shock shape, and vorticity intensity) are also greatly iufluenced by the shock oscillation due to acoustic waves.

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고에너지펄스를 이용한 충격파 발생과 응용 (Laser Supported Combustion Waves and Plasma Flows)

  • 이현희;최지혜;곽민철;여재익
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2007년도 제34회 KOSCO SYMPOSIUM 논문집
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    • pp.27-30
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    • 2007
  • We have been setting up experiments on propagation of shock waves generated by the pulsed laser ablation. One side of a thin metal foil is subjected to laser ablation as a shock wave is generated from a localized spot of high intensity energy source. The resulting reactive shock wave, which penetrates through the foil is reflected by an acoustic impedance which causes the metal foil to high-strain rate deform. This short time physics is captured on an ICCD camera. The focus of our research is generating reactive shock wave and high strain rate deforming of thin metal foil for accelerating micro-particles to a very high speed on the orders of several thousand meter per second. Somce innovative applications of this device will be discussed.

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초소형 EFI 착화기의 비행편 특성에 따른 충격파 감쇠 연구 (A Study on Shock Attenuation according to the Flyer Characteristics of a Subminiaturized EFI detonator)

  • 유현주;김보훈;장승교;김규형;여재익
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.426-432
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    • 2017
  • 충격에 의한 초소형 EFI 착화기의 기폭 성능을 규명하기 위하여 초소형 비행편 충돌 시 발생되는 고체 내 충격 감쇠에 대한 실험 및 수치해석을 수행함으로써 비행편의 충돌 속도와 하중을 계산하였다. 본 연구를 통하여 비행특성에 따른 충격파 강도 및 지속 시간을 결정함으로써 초소형 파이로테크닉 장치의 착화를 위한 비행편의 임계 속도의 예측 가능성을 확인하였다.

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터빈축차내에 내재된 타원균열의 응력세기계수 결정 (Determination of Stress Intensity Factors for Embedded Elliptical Crack in Turbine Rotor)

  • 이강용;김종성;하정수
    • 대한기계학회논문집
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    • 제19권5호
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    • pp.1229-1242
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    • 1995
  • The thermal shock stress intensity factors of semi-elliptical surface crack in finite plate and the stress intensity fractors of embedded elliptical crack in turbine rotor is determined by means of Vainshtok weight function method. In case of semi-elliptical surface crack, the solution is compared with previous solution. The stress intensity factor for embedded elliptical crack in turbine rotor loaded by centrifugal and thermal loading is also determined. In this case, the value of stress intensity factor is larger at crack contour near internal radius surface and is almost constant at the crack contour farther from internal radius surface.

비후성 반흔 각질세포와 정상 각질세포의 유전자 비교분석 (Difference of Gene Expression between Hypertrophic Scar Keratinocytes and Normal Keratinocytes)

  • 최성원;정호윤;임영국;김훈남;오지원;김문규;전세화;홍용택
    • Archives of Plastic Surgery
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    • 제37권4호
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    • pp.317-322
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    • 2010
  • Purpose: There is no clear evidence of the original cause of hypertrophic scar, and the effective method of treatment is not yet established. Recently the steps of searching in gene and molecular level are proceeding. we are trying to recognize the difference between keratinocytes of hypertrophic scar and normal skin. Then we do support the comprehension of the scar formation mechanism and scar management. Methods: Total RNAs were extracted from cultured keratinocytes from 4 hypertrophic scars and normal skins. The cDNA chips were prepared. A total of 3063 cDNAs from human cDNA library were arrayed. And the scanning data were analyzed. Results: On microarray, heat shock protein, pyruvate kinase, tumor rejection antigen were more than 2 fold intensity genes. Among them, heat shock 70 kd protein showed the strongest intensity difference. Conclusion: In this study, it can be concluded that heat shock proteins play an important role in the process of wound healing and scar formation. This study provides basic biologic information for scar research. The new way of the prevention and treatment of scar formation would be introduced with further investigations.

가스 연료와 공기 혼합물 내 압력파와 화염의 상호 작용에 의한 연소폭발천이 현상 연구 (Deflagration to detonation transition by interaction between flame and shock wave in gas mixture)

  • 곽민철;여재익
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.369-374
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    • 2010
  • 본 연구에서는 가스 연료와 공기 혼합물 내 압력파에 의해 유도되는 화염 가속과 연소폭발천이 현상을 수치적 계산을 통하여 살펴본다. 실험에 기반을 둔 초기 조건 하에서 점성력, 열전단, 몰질량 확산, 그리고 화학 반응을 고려한 reactive compressible Navier-Stokes 방정식을 사용하여 계산을 수행하였다. 반복되는 압력파와 화염의 상호 작용에 의해 발생되는 화염의 Richtmyer-Meshkov (RM) 불안정성에 의해 증가된 화염면을 통하여 생기는 hot spot들에 의한 폭굉의 발생을 모델링하였다. 또한 압력파의 강도 변화에 따른 연소폭발천이 현상의 변화를 살펴보았다.

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MR 현가장치를 장착한 승용 차량의 진동제어 (Vibration Control of a Passenger Vehicle Featuring MR Suspension Units)

  • 이환수;최승복;이순규
    • 소음진동
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    • 제11권1호
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    • pp.41-48
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    • 2001
  • This paper presents vibration control performance of a passenger vehicle featuring magneto-rheological (MR) suspension units. As a first step, a cylindrical shock absorber is designed and manufactured on the basis of Bingham Property of a commercially available MR fluid. After verifying that the damping force of the shock absorber can be controlled by the intensity of magnetic field(or input current), it is applied to a full-car model. An optimal controller is then formulated to effectively suppress unwanted vibration of the vehicle system. The control performances are evaluated via hardware-in-the-loop simulation(HILS), and presented in both time and frequency domains.

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원자로 용기의 가압열충격에 대한 파괴역학 해석 - 탄소성 거동과 클래드부의 영향 - (Fracture Mechanics Analysis of Reactor Pressure Vessel Under Pressurized Thermal Shock-The Effect of Elastic-Plastic Behavior and Stainless Steel Cladding-)

  • 주재황;강기주;정명조
    • 대한기계학회논문집A
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    • 제26권1호
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    • pp.39-47
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    • 2002
  • Performed here is an assessment study for deterministic fracture mechanics analysis of a pressurized thermal shock(PTS). The PTS event means an event or transient in pressurized water reactors(PWRs) causing severe overcooling(thermal shock) concurrent with or followed by significant pressure in the reactor vessel. The problems consisting of two transients and 10 cracks are solved and maximum stress intensity factors and maximum allowable nil-ductility reference temperatures are calculated. Their results are compared each other to address the general characteristics between transients, crack types and analysis methods. The effects of elastic-plastic material behavior and clad coating on the inner surface are explored.