• 제목/요약/키워드: large- amplitude

검색결과 783건 처리시간 0.027초

ENO기법을 이용한 연소 엔진 흡기계 소음의 방사에 관한 수치적 연구 (Numerical Study on the Radiation of Intake Noise from Internal Combustion Engine by Using Essentially Non-Oscillatory Schemes)

  • 김용석;이덕주
    • 소음진동
    • /
    • 제8권2호
    • /
    • pp.239-250
    • /
    • 1998
  • Traditionally, intake noise from internal combustion engine has not recevied much attention compared to exhaust noise. But nowadays, intake noise is a major contributing factor to automotive passenger compartment noise levels. The main objective of this paper is to identify the mechanism of generation, propagation and radiation of the intake noise. With a simplest geometric model, one of the main noise sources for the intake stroke is found to be the pressure surge, which is generated after intake valve closing. The pressure surge, which has the nonlinear acoustic behavior, propagates and radiates with relatively large amplitude. In this paper, unsteady compressible Navier-Stokes equations are employed for the intake stroke of axisymmetric model having a single moving cylinder and a single moving intake valve. To simulate the periodic motion of the piston and the valve, unsteady deforming mesh algorithm is employed and Thompson's non-reflecting boundary condition is applied to the radiation field. In order to resolve the small amplitude waves at the radiation field, essentially non-oscillatory(ENO) schemes with an artificial compression method (ACM) are used.

  • PDF

로켓연소기에서 최적의 감쇠특성을 보이는 분사기형 배플의 간극 검증을 위한 상압모사연소시험 (Simulating Combustion Tests for the Verification of Baffle Gap of Optimal Damping Characteristics in Liquid Rocket Combustors)

  • 김홍집;이광진;최환석
    • 한국항공우주학회지
    • /
    • 제36권2호
    • /
    • pp.179-185
    • /
    • 2008
  • 분사기형 배플이 설치된 연소기에 대하여 최적의 감쇠를 가지는 배플간극을 모사연소시험을 통하여 최종적으로 검증하였다. 연소실에서 압력섭동의 최대진폭과 연소안정성 여분을 통하여 배플에 의한 감쇠능력을 정량화하였다. 본 연구의 결과가 상온음향시험에서의 결과와 정성적으로 동일함을 파악할 수 있었다. 배플 간극에 있어서도 상온음향시험과 동일한 간극에서 최적의 연소안정성 여분을 가짐을 확인하였다. 이러한 연소장과의 상호작용을 고려한 결과는 배플의 길이 및 간극의 결정에 매우 유용한 자료를 제공하여 실제 연소기 설계 및 조립에 지침으로서 적용될 수 있을 것이다.

실측 파형과 수치 파형에 의한 진동주응력 비교 (Comparison of the Vibration Principal Stress by Experimental and Numerical Waveform)

  • 홍웅기;송정언;박영민
    • 환경영향평가
    • /
    • 제21권5호
    • /
    • pp.609-615
    • /
    • 2012
  • In recent years, the development of computer technique was possible to the simulation analysis of the structure caused by ground vibration. Generally, finite element method(FEM) has been used in these structural analysis. In this study, it was calculated to the vibration energy as measuring vibration waveform, and estimated about principal stress due to medium characteristics of the ground as processing dynamic analysis by the vibration energy. The results are as follows : Firstly, the principal stress distribution in all mediums was different due to a medium condition, and the principal stress at concrete medium was represented to difference due to physical characteristics. Secondly, the principal stress by time increasing was represented to maximum amplitude within 0.03 second. And also, the principal stress after maximum amplitude was very large at concrete medium, which was considered to be formed compression or tension range at a medium boundary. Thirdly, the variation of principal stress at concrete medium was represented in the order of RC medium, NC=H medium, NC=S medium. It was considered that the vibration energy propagated fast when a medium have a big elasticity and density.

Fatigue behavior of stud shear connectors in steel and recycled tyre rubber-filled concrete composite beams

  • Han, Qing-Hua;Wang, Yi-Hong;Xu, Jie;Xing, Ying
    • Steel and Composite Structures
    • /
    • 제22권2호
    • /
    • pp.353-368
    • /
    • 2016
  • This paper extends our recent work on the fatigue behavior of stud shear connectors in steel and recycled tyre rubber-filled concrete (RRFC) composite beams. A series of 16 fatigue push-out tests were conducted using a hydraulic servo testing machine. Three different recycled tyre rubber contents of concrete, 0%, 5% and 10%, were adopted as main variable parameters. Stress amplitudes and the diameters of studs were also taken into consideration in the tests. The results show that the fatigue lives of studs in 5% and 10% RRFC were 1.6 and 2.0 times greater of those in normal concrete, respectively. At the same time, the ultimate residual slips' values of stud increased in RRFC to highlight its better ductility. The average ultimate residual slip value of the studs was found to be equal to a quarter of studs' diameter. It had also been proved that stress amplitude was inversely proportional to the fatigue life of studs. Moreover, the fatigue lives of studs with large diameter were slightly shorter than those of smaller ones and using larger ones had the risk of tearing off the base metal. Finally, the comparison between test results and three national codes was discussed.

케이블댐퍼 감쇠성능의 수치해석적 연구 (Numerical Analysis Study on Damping Performance of Cable Damper)

  • 임성순
    • 복합신소재구조학회 논문집
    • /
    • 제6권2호
    • /
    • pp.97-104
    • /
    • 2015
  • Compared with a strong axial rigidity due to large intial tension, cable has a weak laterally flexural rigidity. A variety of dynamic loads such as traffic loads and wind loads etc. cause the cables to vibrate significantly and affect the mechanical properties and the performance of cables. Therefore, vibration reduction design is an urgent task to control the vibration of cable-supported bridges. Because a various kind of dampers have shown to reduce the amplitude and duration time of vibration of cable from measured date in field test, damper can be considered that it is effective device significantly to reduce the amplitude and duration time in vibration of cable. Vibration characteristics of cable can change according to manufacturing method and type of established form, and damper has been designed according to distribution of natural frequencies and vibration modes. In this study, numerical analysis is used to show the reduction effects of vibrations and present the design of damper for vibration reduction of cable.

액체 로켓엔진의 연소 안정성 평가 (Stability Rating of Liquid Propellant Rocket Engine)

  • 손채훈;김영목
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2003년도 제21회 추계학술대회 논문집
    • /
    • pp.73-77
    • /
    • 2003
  • 액체 로켓엔진 개발과정에서 수행되는 여러 가지 시험 중 연소 안정성 평가 시험을 통해, KSR-III 로켓엔진의 연소 안정성을 평가하였다. 안정성 평가시험에서, 엔진이 외부 교란에 의한 압력 진통을 감쇠시켜 본래의 안정한 연소로 회복되는 경우, 그 엔진은 연소 안정화 능력을 가지고 있다고 판정할 수 있다. 로켓엔진은, 교란의 크기를 예측하기 어려운 외부 섭동에 노출될 수 있으므로, 엔진의 연소 안정화 가능 여부를 확인하는 것과 더불어 엔진이 갖고 있는 연소 안정화 능력을 정량화하여 파악하는 작업이 필요하다. 이를 위해 몇 가지 인자를 도입하였고, 이를 평가하는 방법을 검토하였다. 성공적으로 완료된 KSR-III 로켓개발과정에서 로켓엔진의 안정성 확보를 위해 5회의 안정성 평가 시험이 수행되었다. 이를 토대로, 앞서 언급한 안정화 능력의 정량화 방법을 KSR-III 엔진에 적용하여 그 엔진의 안정화 성능을 분석하였다.

  • PDF

Statistical analysis of SC-associated geosynchronous magnetic field perturbations

  • 김관혁;박종선;이동훈;진호
    • 천문학회보
    • /
    • 제37권1호
    • /
    • pp.91.2-91.2
    • /
    • 2012
  • Kokubun (1983) reported the local time variation of normalized amplitude of sudden commencement (SC) with a strong day-night asymmetry at geosynchronous orbit with 81 SC events. Further careful inspection of Kokubun's local time distribution reveals that the normalized SC amplitudes in the prenoon sector are larger than those in the postnoon sector. That is, there is a morning-afternoon asymmetry in the normalized SC amplitudes. Until now, however, there are no studies on this SC-associated morning-afternoon asymmetry at geosynchronous orbit. Motivated by this previous observation, we investigate a large data set (422 SC events in total) of geosynchronous SC observations and confirm that the geosynchronous SC amplitudes is larger in the morning sector than in the afternoon sector. This morning-asymmetry is probably caused by the enhancement of partial ring current, which is located in the premidnight sector, due to solar wind dynamic pressure increase. We also examine the latitudinal and seasonal variations of the normalized SC amplitude. We find that the SC-associated geosynchronous magnetic field perturbations are dependent on the magnetic latitude and season of the year. This may be due to the location of the magnetopause and cross-tail currents enhanced during SC interval with respect to geosynchronous spacecraft position.

  • PDF

평판에 충돌하는 초음속 제트에 유동특성 (Characteristics of Supersonic Jet Impingement on a Flat Plate)

  • 홍승규;이광섭;박승오
    • 한국전산유체공학회지
    • /
    • 제6권3호
    • /
    • pp.32-40
    • /
    • 2001
  • Viscous solutions of supersonic jet impinging on a flat plate normal to the flow are simulated using three-dimensional Navier-Stokes solver. The jet impinging flow structure exhibits such complex nature as shock shell, plate shock and Mach disk depending on the flow parameters. Among others, the dominant parameters are the ratio of the nozzle exit pressure to the ambient pressure and the distance between the nozzle exit plane and the impinging plane. In the present study, the nozzle contour and the pressure ratio are held fixed, while the jet impinging distance is varied to illuminate the characteristics of the jet plume with the distance. As the plate is placed close to the nozzle at 3D high, the computed wall pressure at or near the jet center oscillates with large amplitude with respect to the mean value. Here D is the nozzle exit diameter. The amplitude of wall pressure fluctuations subsides as the distance increases, but the maximum mean pressure level at the plate is achieved when the distance is about 4D high. The frequency of the wall pressure is estimated at 6.0 kHz, 9.3 kHz, and 10.0 kHz as the impinging distance varies from 3D, 4D, to 6D, respectively.

  • PDF

반경비 및 각속도의 변화에 따른 Taylor 유동에 관한 연구 (A STUDY ON TAYLOR FLOW ACCORDING TO RADIUS RATION AND ANGULAR VELOCITY)

  • 배강열;김형범;정희택
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2007년도 추계 학술대회논문집
    • /
    • pp.127-133
    • /
    • 2007
  • This paper represents the numerical study on Taylor flow according to the radius ratio and the angular velocity for flow between tow cylinder. The numerical model is consisted of two cylinder which inner cylinder is rotating and outer cylinder is fix, and the axial direction is used the cyclic condition because of the length for axial direction is assumed infinite. The diameter of inner cylinder is assumed 86.8 mm, the numerical parameters are angular velocity and radius ratio. The numerical method is compared with the experimental results by Wereley, and the results are very good agreement. The critical Taylor number is calculated by theoretical and numerical analysis, and the results is showed the difference about ${\pm}10\;%$. As $Re/Re_c$ is increased, Taylor vortex is changed to wavy vortex, and then the wave number for azimuthal direction is increased. Azimuthal wave according to the radius ratio is showed high amplitude and low frequence in case of small radius ratio, and is showed low amplitude and high frequence in case of large radius ratio.

  • PDF

Nonlinear vibration properties of a zigzag single-walled carbon nanotube embedded in a polymer matrix

  • Besseghier, Abderrahmane;Heireche, Houari;Bousahla, Abdelmoumen Anis;Tounsi, Abdelouahed;Benzair, Abdelnour
    • Advances in nano research
    • /
    • 제3권1호
    • /
    • pp.29-37
    • /
    • 2015
  • In the current study, the nonlinear vibration properties of an embedded zigzag single-walled carbon nanotube (SWCNT) are investigated. Winkler-type model is used to simulate the interaction of the zigzag SWCNTs with a surrounding elastic medium. The relation between deflection amplitudes and resonant frequencies of the SWCNT is derived through harmonic balance method. The equivalent Young's modulus and shear modulus for zigzag SWCNT are derived using an energy-equivalent model. The amplitude - frequency curves for large-amplitude vibrations are graphically illustrated. The simulation results show that the chirality of zigzag carbon nanolube as well as surrounding elastic medium play more important roles in the nonlinear vibration of the single-walled carbon nanotubes.