• 제목/요약/키워드: shock wave attenuation

검색결과 24건 처리시간 0.02초

MR Insert 의 충격저감 성능 연구 (A Study on MR Insert for Shock Wave Attenuation)

  • 강병우;김재환;최승복;김경수
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2001년도 춘계학술대회논문집
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    • pp.121-126
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    • 2001
  • This paper presents the experimental study for the reduction of transmitted shock waves in smart structures incorporating MR insert. MR fluid is filled within the two aluminum layers and two piezoceramic disks are embedded on the host plate as a transmitter and a receiver of the shock wave. Pulse wave generated by the transmitter is transmitted to the receiver through the MR insert and the plate. By applying magnetic field to the MR insert, the amplitude of the transmitted shock wave is reduced remarkably. The attenuation performance is tested by changing the applied magnetic field on MR inserts in two ways: by changing angle of permanent rubber magnet from 90 to 5 with 5 decrements, by using electromagnet in which magnetic field is controllable. The propagating wave speed of MR insert is also investigated.

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직관내를 전파하는 압축파의 감쇠와 변형에 관한 수치해석적 연구 (Numerical study on attenuation and distortion of compression wave propagation into a straight tube)

  • 김희동
    • 대한기계학회논문집B
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    • 제20권7호
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    • pp.2315-2325
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    • 1996
  • A compression wave is attenuated or distorted as it propagates in a tube. The present study investigated the propagation characteristics of the compression waves which are generated by a train in a high-speed railway tunnel. A Total Variation Diminishing (TVD) difference scheme was applied to one-dimensional, unsteady viscous compressible flow. The numerical calculation involved the effects of wall friction, heat transfer and energy loss due to the friction heat in the boundary layer behind the propagating compression wave, and compared with the measurement results of a shock tube and a real tunnel. The present results show that attenuation of the compression wave in turbulent boundary layer is stronger than in laminar boundary layer, but nonlinear effect of the compression wave is greater in the laminar boundary layer. The energy loss due to the frictional heat had not influence on attenuation and distortion of the propagating compression waves.

폭발하중으로 부터 지반의 완충적 동과에 대한 수치해석적 연구 (Numerical Analysis of Ground Shock Attenuation from Explosive Loading)

  • 박종관
    • 한국지반공학회지:지반
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    • 제4권4호
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    • pp.19-28
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    • 1988
  • An underground explosion crests shock waves, which propagate to a buried structure through the이 ground. Due to the explosion, very high stresses and large deformation occur in the ground so that the shock waves decay gradually. In this study the numerical simulation of the ground shock attenuation has teen performed. One dimensional wave equation is presented and the finite difference method is applies. A Cap model is adopted to describe the stress-strain behavior of the ground. The results are expressed by the attenuation of the peak stress and the particle vrelocity by the time and the distance.

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고속철도 터널에서 발생하는 파동현상에 관한 충격파관의 연구(2)-압축파의 감쇠와 비선형효과- (Study of Shock Tube for Wave Phenomenon in High Speed Railway Tunnel(II)-attenuation and Nonlinear Effect of Compression Waves-)

  • 김희동;송미일태
    • 대한기계학회논문집
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    • 제19권8호
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    • pp.1972-1981
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    • 1995
  • As a railway train enters a tunnel at high speed, a compression wave is formed in front of the train and propagates along the tunnel. The compression wave subsequently emerges from the exit of the tunnel, which causes an impulsive noise. The impulsive noise is closely related to the pressure gradient of the compression wave propagating the tunnel. In order to investigate the characteristics of the compression waves, in the present study an experiment was made using a shock tube. The results show that the strength of a compression wave decreases with the distance from the tunnel entrance and the nonlinear effect of compression wave appears to be significant if strength of the initial compression wave is greater than 7 kPa. Furthermore if the wave pattern is known, attenuation of the compression wave propagating in a tunnel can be reasonably predicted by a theoretical equation considering viscous action and heat transfer in boundary layer.

STS 격벽착화기의 충격파 감쇠 특성 해석 (Analysis on Shock Attenuation of STS Bulkhead Initiator)

  • 김보훈;장승교;여재익
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.440-444
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    • 2017
  • 격벽착화기의 기폭으로 인하여 발생하는 충격파가 격벽을 통과할 때의 감쇠 특성을 해석하기 위하여 2차원 하이드로다이나믹 해석을 수행하였다. HNS와 HMX가 적층되어 있는 기폭제와 STS 격벽간의 연동해석을 통해 폭압 생성 및 압력파 감쇠 현상을 정밀하게 모사하였다. VISAR로 측정한 시험 데이터와의 정량적인 비교를 위하여 격벽 끝단에서의 자유표면 속도를 계측하였다. 해석결과, 격벽 두께에 따른 충격파의 압력 감쇠 패턴이 지수적으로 감소하는 것을 확인하였으며, 시간에 따라 측정된 입자속도에서 관찰된 변곡 패턴은 기폭부와 격벽 사이의 충전면의 급격한 파쇄(spallation)에 의한 충격파의 잇따른 전파에 의한 것임을 규명하였다.

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Numerical Prediction of the Flow Characteristics of a Micro Shock Tube

  • ;;김희동
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.178-181
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    • 2011
  • Recently, micro shock tube is being extensively used in various fields of engineering applications. The flow characteristics occurring in the micro shock tube may be significantly different from that of conventional macro shock tube due to very low Reynolds number and Knudsen number effects which are, in general, manifested in such flows of rarefied gas, solid-gas two-phase, etc. In these situations, Navier-Stokes equations cannot properly predict the micro shock tube flow. In the present study, a two-dimensional CFD method has been applied to simulate the micro shock tube, with slip velocity and temperature jump boundary conditions. The effects of wall thermal conditions on the unsteady flow in the micro shock tube were also investigated. The unsteady behaviors of shock wave and contact discontinuity were, in detail, analyzed. The results obtained show much more attenuation of shock wave, compared with macro-shock tubes.

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내리막 달리기의 충격 쇼크와 신체 관절의 운동학적 특징 (Impact shock and kinematic characteristics of the lower extremity's joint during downhill running)

  • 류지선
    • 한국운동역학회지
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    • 제15권4호
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    • pp.117-129
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    • 2005
  • The purpose of this study was to characterize the impact shock wave and its attenuation, and the kinematic response of the lower extremity's joints to the impact shock during downhill running in which the lower extremity's extensor acts dominantly. For this study, fifteen subjects(mean age:$27.08{\pm}4.39$; mass:$76.30{\pm}6.60$; height:$177.25{\pm}4.11$) were required to run on the 0% grade treadmill and downhill grades of 7%, and 15% in random at speed of their preference. When the participant run, acceleration at the tibia and the sacrum and kinematic data of the lower extremity were collected for 20s so as to provide at least 5 strides for analysis at each grade. Peak impact accelerations were used to calculate shock attenuation between the tibia and sacrum in time domain at each grade. Fast Fourier transformation(FFT) and power spectral density(PSD) techniques were used to analyze impact shock factors and its attenuation in the frequency domain. Joint coordinate system technique was used to compute angular displacement of the ankle and knee joint in three dimension. The conclusions were drawn as fellows: 1. Peak impact accelerations of the tibia and sacrum in downhill run were greater than that of 0% grade run, but no significant between conditions. Peak shock of PSD resembled also in pattern of peak impact acceleration. The wave of impact shock attenuation between the tibia and sacrum decreased with increasing grade, but didn't find a significant difference between grade conditions. 2. Adduction/abduction, flexion/extention, and internal/external rotation of the ankle and knee joints at support phase between grade conditions didn't make much difference. 3. At grade of 7% and 15%, there were relationship between the knee of the flexion/extension movement and peak impact acceleration during heel strike and found also it in the ankle of plantar/dorsiflexion at grade of 15%.

MR Insert를 이용한 구조물의 응력파 저감 (Stress Wave Reduction of Structures Using MR Inserts)

  • 강병우;김재환;최승복;김경수
    • 한국소음진동공학회논문집
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    • 제11권4호
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    • pp.71-77
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    • 2001
  • In this paper, stress wave propagation characteristics of MR(Magneto-rheological) inserts are experimentally investigated. Generally, stress waves of structures such as warships or submarines are induced by shock waves from underwater explosion. Their fatal effects on the shipboard equipments or structures damage the performance of warships. But, such a problem can be solved by controlling the stress waves propagating through structures by means of MR inserts. MR insert consists of two aluminum layers and MR fluid filled in between. Two piezoceramic disks are embedded on the host plate as a transmitter and a receiver of stress waves. Pulse waves are generated by the transmitter and they reach to the receiver through the MR insert. Permanent magnet and magnetic coil are used to produce magnetic field at the MR insert. In the presence of magnetic field, MR particles are arranged in chains parallel to the magnetic field such that the transmitted stress waves are reduced. Attenuation of stress waves is experimentally investigated.

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다공벽을 이용한 충격파 강도의 피동제어 (Passive control of strength of shock wave)

  • 최영상;권순범;조철영
    • 대한기계학회논문집B
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    • 제21권1호
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    • pp.174-184
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    • 1997
  • A shock wave, being an irreversible process, gives rise to entropy increase. A great deal of effort has been made to control shock wave and boundary layer interaction related to energy losses as well as problems of vibration and noise. In the present study, tests are performed on a roof mounted half circular arc in an indraft type supersonic wind tunnel to evaluate the effects of porosity, length and depth of cavity in passive control of shock wave on the attenuation of shock strength by reviewing the measured static pressures at the porous wall and cavity. Also the flow field is visualized by a Schlieren system. The results show that in the present study the porosity of 8% produced the largest reduction of pressure fluctuations and that for the same porosity, the strength of shock wave decreases with the increasings of the depth and length of cavity.

How Shock Wave Interacts with a Vortex ?

  • Chang Keun-Shik;Chang Se-Myong
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2004년도 춘계학술대회 논문집
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    • pp.1-7
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    • 2004
  • When a vortex diffracts upon encountering a vortex, many strong and weak waves are produced in the course of interaction. They are the cause of shock wave attenuation and noise production. This phenomenon is fundamental to understanding the more complex supersonic turbulent Jet noise. In this paper we have reviewed the research on shock-vortex interaction we have carried on last seven years. We have computationally investigated the parameter effect. When a shock is strong, shock diffraction pattern becomes complex since the slip lines from the triple points on Mach stem curl into the vortex, causing an entropy layer. When the vortex is unstable, vortexlets are brought about each of which make shock diffraction of a reduced intensity. Strong vortex produces quadrupole noise as it impinges into a vortex. Elementary interaction models such as shock splitting, shock reflection, and shock penetration are presented based on shock tube experiment. These models are also verified by computational approach. They easily explain production and propagation of the aforementioned quadrupole noise, Diverging acoustics are explained in terms of shock-vortexlet interactions for which a computational model Is constructed.

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