• 제목/요약/키워드: Dynamic damping coefficients

검색결과 196건 처리시간 0.142초

동심환내의 회전체 진동에 의한 부가질량, 유체감쇠계수 및 유체탄성계수에 관한 연구 (Added Mass, Viscous Damping and Fluid-stiffness Coefficients on the Rotating Inner Cylinder in Concentric Annulus)

  • 심우건;박진호;김기선
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2001년도 춘계학술대회논문집
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    • pp.695-701
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    • 2001
  • While a rotating inner cylinder executes a periodic translational motion in concentric annulus, the vibration of the rotating inner cylinder is induced by fluid-dynamic forces acting on the cylinder. In the previous study related to journal bearing, the unsteady viscous flow in the annulus and the fluid-dynamic forces were evaluated based on a numerical approach. Considering the dynamic-characteristics of unsteady viscous flow, an approximate analytical method has been developed for estimating added mass, viscous damping and fluid-stiffness coefficients. For the study of flow-induced vibrations and related instabilities, it is of interest to separate the coefficients from the fluid-dynamic forces. The added-mass and viscous damping coefficients for very narrow annular configurations, as journal bearing. can be approximated by considering the gap ratio to the radius of inner cylinder, while the fluid-stiffness coefficient is related to the Reynolds number, the oscillatory Reynolds number and the gap ratio.

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비정상 Euler 방정식을 이용한 동안정 미계수 예측 (Prediction of Dynamic Stability Derivatives Using Unsteady Euler Equations)

  • 박수형;김윤식;권장혁
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2001년도 춘계 학술대회논문집
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    • pp.78-84
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    • 2001
  • A dual-time stepping algorithm combined with a parallelized multigrid DADI method is presented to predict the dynamic damping coefficients. The Basic Finner model is chosen to validate the prediction capability of the present unsteady Euler method. The linearity of the pitch- and roll-damping coefficients is shown in the low angular rates and the interesting large drop and stiff increment in transonic region for roll-damping coefficients are explained in detail. Through the analysis for the pressure distributions at Mach number 1.0 to 1.2, the sudden drop results from the normal shock and the stiff increment of roll-damping reflects the transition of the normal shock to the oblique shock. The results also show that the Euler equations can give the damping coefficients with a comparable accuracy.

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공작기계 주축계의 진동특성해석에 관한 연구 (Dynamic Characteristics Analysis of a Machine-Tool Spindle System)

  • 김석일;곽병만;이후상;정재호
    • 한국정밀공학회지
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    • 제8권2호
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    • pp.57-68
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    • 1991
  • In this study, to analyse the dynamic characteristics of a machine-tool spindle system, the spindle is mathematically represented by a Timoshenko beam including the internal damping of beam material, and each bearing by four bearing coefficients; stiffness and damping coefficients in moment and radial directions. And the dynamic compliance of the system is calculated by introducing the transfer matrix method, and the complex modal analysis method has been applied for the modal parameter identification. The influence of the bearing coefficients, material damping factor and bearing span on the dynamic characteristics of the system is parametrically examined.

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비행선의 동적 감쇠계수 계산 방법에 관한 연구 (A Study of Computation Methods for Dynamic Damping Coefficients of an Airship)

  • 박수형;장병희;김유진;권장혁
    • 한국항공우주학회지
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    • 제31권5호
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    • pp.10-17
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    • 2003
  • 정적으로 불안정한 비행선의 안전성을 확보하기 위해서는 동적 안정성이 필수적으로 요구된다. 본 연구에서는 강제진동 풍동시험을 보완하고 검증하기 위한 수치해석이 수행되었다. 비행선의 저속 유동장 해석을 위해 저마하수 예조건화된 수치기법이 적용되었다. 동적 감쇠계수의 변화를 두 가지 계산방법을 적용해 살펴보았다. 계산결과, 비행선은 각 방향의 모멘트에 대해 동적으로 안정되고, 힘에 대해서는 불안정하게 나타났다. 또한, 감쇠계수는 받음각과 각속도의 크기에 대한 영향보다 회전방향에 대한 영향이 더 큼을 확인하였다.

동적 시간이력 탄소성 지진 해석을 위한 레일레이 감쇠계수 결정방법 고찰 (Investigation on the Determination Method of Rayleigh Damping Coefficients for Dynamic Time History Elastic-Plastic Seismic Analysis)

  • 김종성;이석현;권형도;오창영
    • 한국압력기기공학회 논문집
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    • 제13권2호
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    • pp.38-43
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    • 2017
  • This paper investigates how to determine the Rayleigh damping coefficients for dynamic time history seismic analysis of piping systems. Three methods are applied. The first one is a conventional method to use the natural frequencies of the mode 1 and 2, derived from dynamic analysis. The second method is to determine the Rayleigh damping coefficients based on frequency range of the acceleration histories. The last one is a iterative transient response analysis method using the transient analysis results without and with damping. It is found that the conventional method and the iterative transient response method yield the same results whereas the acceleration frequency-basis method provides more conservative result than the other methods. In addition, it is concluded that the iterative transient response method is recommended.

Theoretical research on the identification method of bridge dynamic parameters using free decay response

  • Tan, Guo-Jin;Cheng, Yong-Chun;Liu, Han-Bing;Wang, Long-Lin
    • Structural Engineering and Mechanics
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    • 제38권3호
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    • pp.349-359
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    • 2011
  • Input excitation and output response of structure are needed in conventional modal analysis methods. However, input excitation is often difficult to be obtained in the dynamic load test of bridge structures. Therefore, what attracts engineers' attention is how to get dynamic parameters from the output response. In this paper, a structural experimental modal analysis method is introduced, which can be used to conveniently obtain dynamic parameters of the structure from the free decay response. With known damping coefficients, this analysis method can be used to identify the natural frequencies and the mode shapes of MDOF structures. Based on the modal analysis theory, the mathematical relationship of damping ratio and frequency is obtained. By using this mathematical relationship to improve the previous method, an improved experimental modal analysis method is proposed in this paper. This improved method can overcome the deficiencies of the previous method, which can not identify damping ratios and requires damping coefficients in advance. Additionally, this improved method can also identify the natural frequencies, mode shapes and damping ratios of the bridge only from the free decay response, and ensure the stability of identification process by using modern mathematical means. Finally, the feasibility and effectiveness of this method are demonstrated by a numerical example of a simply supported reinforced concrete beam.

2열 원주 그루브 급기 저어널 공기베어링의 해석 (Analysis of the Air Journal Bearings with Two Circumferential Grooves)

  • 박상신;안유민;한동철
    • Tribology and Lubricants
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    • 제13권4호
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    • pp.40-46
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    • 1997
  • The externally pressurized air journal bearings which have two circumferential grooves with inherently compensated restrictors are analyzed. Two circumferential grooves with restrictors are made on the bearing surface in order to increase the stiffness and damping coefficients. In this paper, the dynamic characteristics such as stiffness and damping coefficients of this type of bearings are calculated. As a result of theoretical analysis, it is verified that there exist the groove depth and the distance between two grooves which generate the maximum stiffness at the given bearing dimensions.

자유진동기법을 이용한 공대지 미사일의 동안정성에 관한 연구 (A Study on the Dynamic Stability of Air-to-Ground Missile Using the Free Vibration Technique)

  • 박재현;백승욱;조환기;허원욱
    • 한국군사과학기술학회지
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    • 제2권2호
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    • pp.61-69
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    • 1999
  • A dynamic stability test was performed to determine dynamic stability derivatives for the pure pitching motion of air-to-ground missile model in the low speed wind tunnel. The free vibration technique was employed to acquire oscillation characteristics of the model for damping coefficients. Damping coefficients are obtained by the method of logarithmic decrement. Results show good damping effects and stability capability at Mach numbers 0.1 and 0.2, with the angle of attack ranging from -15 to +20 degrees.

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정상 운동을 이용한 발사체의 동적 감쇠계수 계산 (Computation of Dynamic Damping Coefficients for Projectiles using Steady Motions)

  • 박수형;권장혁
    • 한국항공우주학회지
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    • 제31권8호
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    • pp.19-26
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    • 2003
  • 비정상 Euler 방정식 틀에서 동안정 미계수의 정상 예측 방법을 제안하였다. 새로운 접근방법은 비정상 지배방정식을 수정하지 않고 정상 예측방법을 적용하도록 해 준다. 제안된 방법을 통해 lunar 코닝운동 및 나선운동을 사용하여 피치감쇠 계수 합과 개별 값을 계산하였다. ANSR 형상과 Basic Finner 형상에 대한 계산결과는 PNS 계산결과, 실험치, 그리고 비정상적 예측방법을 사용한 결과와 잘 일치하고, 직교좌표계에서 정상적 예측 방법이 피치감쇠 계수의 예측에 성공적으로 적용될 수 있음을 보여준다.

온도상승 및 난류효과를 고려한 대형 틸팅패드 저널베어링의 동특성 해석 (Dynamic Analysis of a Large Tilting Pad Journal Bearing Including the Effects of Temperature Rise and Turbulence)

  • 하현천;김경웅
    • 대한기계학회논문집
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    • 제19권2호
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    • pp.313-321
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    • 1995
  • The effects of the temperature rise and the turbulence are very important factors to predict the accurate performance of a large tilting pad journal bearing. In this study, the dynamic characteristics of a large tilting pad journal bearing are analyzed, taking into account the three dimensional variation of lubricant viscosity and turbulence. The effects of the temperature rise and the turbulence on the stiffness and damping coefficients are investigated in comparison with the results from the laminar or isothermal theory. The stiffness and damping coefficients increase due to the turbulence but decrease due to the temperature rise. The results show that the effects of both the temperature rise and turbulence must be considered simultaneously in order to predict the dynamic characteristics of a large tilting pad journal bearing more accurately.