• 제목/요약/키워드: Velocity ratio

검색결과 2,666건 처리시간 0.039초

응답예측모델을 이용한 속도의존형 감쇠장치의 최대제어력 산정 (Maximum Control Force of Velocity-dependent Damping Devices Using Response Estimation Models)

  • 이상현;민경원
    • 한국소음진동공학회논문집
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    • 제14권6호
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    • pp.503-511
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    • 2004
  • 본 연구에서는 푸리에 모델, 확률 모델, 그리고 Newmark 설계 스펙트럼 방법과 같은 응답예측 모델을 사용하여 속도의존형 감쇠장치에 의해 제어되는 구조물의 응답과 제어기의 최대제어력을 예측하였다. 이를 위해, 유사 속도로부터 실제 속도를 예측하는 방법이 제안되었으며, 이 방법은 감쇠장치에 의해 증가되는 감쇠비의 실제속도에 대한 효과를 고려한다. 시간이력해석결과는 정확한 최대제어력을 예측하기 위해서는 실제속도가 사용되어야 하며, 제안된 방법에 의해 수정된 Newmark 설계 스펙트럼이 가장 전 주기구간에 걸쳐 정확한 예측 값을 산정함을 보여준다.

폭발용접에서 부재의 충돌속도에 관한 실험적 연구 (Experimental Study on the Flyer Velocity in Explosive Welding)

  • 문정기;김청균
    • 대한기계학회논문집
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    • 제17권6호
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    • pp.1423-1430
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    • 1993
  • 본 연구에서는 레이저를 사용한 부재의 충돌속도 계측 실험을 통하여 기존 연구자들의 연구 결과를 비교하고, 이 결과를 바탕으로 보다 간단하고 유용한 실험식 을 제안하고자 한다.

Material Characterization of Weld-Zone Using Poisson's Ratio Distribution

  • Park, Jin-Ha;Kim, Young-H.;Lee, Seung-S.;Kim, Young-Gil
    • 비파괴검사학회지
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    • 제29권6호
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    • pp.586-590
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    • 2009
  • Poisson's ratio, one of elastic constants of elastic solids, has not attracted attention due to its narrow range and difficult measurement. Transverse wave velocity as well as longitudinal wave velocity should be measured for nondestructive measurement of Poisson's ratio. Rigid couplants for transverse wave is one of obstacle for scanning over specimen. In the present work, a novel measurement of Poisson's ratio distribution was applied. Immersion method was employed for the scanning over the specimen. Echo signals of normal beam longitudinal wave were collected, and transverse wave modes generated by mode conversion were identified. From transit time of longitudinal and transverse waves, Poisson's ratio was determined without the information of specimen thickness. Poisson's ratio distribution of the carbon steel weldment was mapped. Heat affected zone of the weldment was clearly distinguished from base and filler metals.

대학 골프선수들의 의도적 지연히팅 시 비거리 결정인자 분석 (An Analysis of decision Factor on Drive Distance for University Golf Player's Object Execution Using Late Hitting Method)

  • 소재무;임영태;김용석;조범욱
    • 한국운동역학회지
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    • 제15권3호
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    • pp.71-78
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    • 2005
  • The purpose of this research was to conduct an analysis on the factors that determine the distance at the time of target swing based on the use of late hitting of outstanding college golfers to verify the difference between late hitting and the distance that target increases in regular swing and the distance. Then, this research conducts an analysis on the correlation between club head velocity, ball velocity, launch angle, back spin, meet ratio and distance that become kinematics variables at the time of target swing. To attain the above mentioned purpose, 25 outstanding college players with average experience and handicap of 6 years and 5, respectively, were targeted Comparative analysis on two swing that target increase in regular and the distance was conducted by used driver. When it pertained to two types of swing. analysis system comprised of an analytical software called the Science Eye of the Bridgestone and peripheries was used to define the relationship between variables of club head velocity, ball velocity, launch angle, back spin, meet ratio that become kinematics variables. As for the method of processing data pertaining to the factors that determine the distance, differences of distance by the type of swing was verified by using independent T-test that leveraged SPSS 120 statistics program. Moreover, level of correlation between variables that contribute to the increase in distance through relation of correlation, and analysis of tendencies was conducted to analyze tendency of non-distance to increase in accordance to the increase of each variable. Key results produced through this experiment are as follows: 1. Artificial late hitting for increased non-distance that targets skilled players had effect on increased the distance(p<. 05). 2 The drive distance is correlated with each measured variable that is positive correlation to ball velocity, club head velocity, meet ratio and relation of back spin and launch angle are negative correlation. ball velocity and club head velocity are very high correlated with drive distance(p<.01), back spin and distance are negative correlation(p<.01). 3. Among each measured variable increasing the club velocity is the most contribution, and ball velocity and meet ratio and the increasing launch angle and back spin is negative effect for increasing distance.

초음파 속도법과 충격반향기법에 의한 콘크리트의 종파 속도 비교 (Comparison of Longitudinal Wave Velocity in Concrete by Ultrasonic Pulse Velocity Method and Impact-Echo Method)

  • 이회근;이광명;김영환
    • 비파괴검사학회지
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    • 제23권2호
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    • pp.98-106
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    • 2003
  • 비파괴시험(NDT)은 구조물의 기능에 손상을 주지 않으면서 콘크리트에 대한 많은 정보를 준다. 여러 가지 NDT 방법들 중에서, 초음파 속도법과 충격반향기법과 같이 탄성파의 속도를 이용하는 방법은 콘크리트의 압축강도, 탄성계수, 포아송비의 추정뿐만 아니라, 내부 미세구조 변화 모니터링과 결함 탐지 등을 위해 이용되고 있다. 본 연구에서는 물-결합재비가 $0.27{\sim}0.50$이고 시멘트 중량의 20%를 플라이 애쉬로 대체 사용한 콘크리트를 제조한 후, 동일한 콘크리트에 대해 초음파 속도법과 충격반향기법을 이용하여 종파 속도를 각각 측정하여 서로 비교하였다. 실험 결과, 콘크리트 공시체로부터 측정된 초음파 속도가 충격반향기법에 의해 측정된 종파 속도, 즉 막대파 속도보다 큰 경향을 나타내었으며, 이들의 차이는 재령이 증가함에 따라 그리고 콘크리트의 강도가 커질수록 각각 감소하는 경향을 나타내었다. 또한, 동포아송비, 정탄성계수, 동탄성계수, 속도-강도의 상관관계 등을 실험적으로 결정하였다. 그 결과, 동적인 방법으로 결정되는 포아송비와 탄성계수가 정적인 시험에 의한 것보다 크게 나타났다. 따라서, 탄성파 속도를 이용하여 콘크리트의 성질들을 보다 정확하게 추정하기 위해서는 속도 특성에 대한 이해가 필요할 것으로 사료된다.

ESTIMATION OF ERRORS IN THE TRANSVERSE VELOCITY VECTORS DETERMINED FROM HINODE/SOT MAGNETOGRAMS USING THE NAVE TECHNIQUE

  • Chae, Jong-Chul;Moon, Yong-Jae
    • 천문학회지
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    • 제42권3호
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    • pp.61-69
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    • 2009
  • Transverse velocity vectors can be determined from a pair of images successively taken with a time interval using an optical flow technique. We have tested the performance of the new technique called NAVE (non-linear affine velocity estimator) recently implemented by Chae & Sakurai using real image data taken by the Narrowband Filter Imager (NFI) of the Solar Optical Telescope (SOT) aboard the Hinode satellite. We have developed two methods of estimating the errors in the determination of velocity vectors, one resulting from the non-linear fitting ${\sigma}_{\upsilon}$ and the other ${\epsilon}_u$ resulting from the statistics of the determined velocity vectors. The real error is expected to be somewhere between ${\sigma}_{\upsilon}$ and ${\epsilon}_u$. We have investigated the dependence of the determined velocity vectors and their errors on the different parameters such as the critical speed for the subsonic filtering, the width of the localizing window, the time interval between two successive images, and the signal-to-noise ratio of the feature. With the choice of $v_{crit}$ = 2 pixel/step for the subsonic filtering, and the window FWHM of 16 pixels, and the time interval of one step (2 minutes), we find that the errors of velocity vectors determined using the NAVE range from around 0.04 pixel/step in high signal-to-noise ratio features (S/N $\sim$ 10), to 0.1 pixel/step in low signa-to-noise ratio features (S/N $\sim$ 3) with the mean of about 0.06 pixel/step where 1 pixel/step corresponds roughly to 1 km/s in our case.

Systemic search for gas outflows in AGNs and star-forming galaxies

  • Woo, Jong-Hak;Son, Donghoon;Bae, Hyun-Jin
    • 천문학회보
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    • 제41권1호
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    • pp.35.2-35.2
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    • 2016
  • We present a census of AGN-driven gas outflows based on the kinematics of ionized gas and stars, using a large sample of ~11,000 emission line galaxies at z < 0.3, selected from SDSS. First, a broad correlation between gas and stellar velocity dispersions indicates that the bulge gravitational potential plays a main role in determining the ionized gas kinematics. However, the velocity dispersion of the [OIII] emission line is larger than stellar velocity dispersion by a factor of 1.3-1.4, suggesting that the non-gravitational (non-virial) component, i.e., outflows, is almost comparable to the gravitational component. Second, gas-to-stellar velocity dispersion ratio increases with both AGN luminosity and Eddington ratio, suggesting that non-gravitational kinematics are clearly linked to AGN accretion. The distribution in the [OIII] velocity - velocity dispersion diagram dramatically expands toward large values with increasing AGN luminosity, implying that the launching velocity of gas outflows increases with AGN luminosity. Third, the fraction of AGNs with a signature of the non-gravitational kinematics, steeply increases with AGN luminosity and Eddington ratio, while the majority of luminous AGNs presents the non-gravitational kinematics in the [OIII] profile. These results suggest that ionized gas outflows are prevalent among type 2 AGNs. On the other hand, we find no strong trend of the [OIII] kinematics with radio luminosity, once we remove the effect of the bulge gravitational potential, indicating that ionized gas outflows are not directly related to radio activity for the majority of type 2 AGNs. We will discuss the implication of these results for AGN feedback in the local universe.

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구리합금그물감의 공극률 및 영각에 의한 유속 감소와 유체역학적 특성에 관한 연구 (A study on flow velocity reduction and hydrodynamic characteristics of copper alloy netting by solidity ratios and attack angles)

  • 강아림;이지훈
    • 수산해양기술연구
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    • 제55권1호
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    • pp.62-73
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    • 2019
  • Recently, copper alloy netting has been proposed as a material for aquaculture facilities that can be set in harsh offshore environments. To design a cage made of copper alloy netting, it is necessary to calculate the flow of water through the netting and force of external sources on the netting. Therefore, this study measured and analyzed the current velocity reduction after passing through the netting and the hydrodynamic forces acting on the netting using copper alloy netting with nine solidity ratios. As a result of the reduction rate of the flow velocity through the netting, the flow reduction rate was increased as the solidity ratio of netting was increased. The flow reduction rate was also increased as the attack angle on the netting was decreased. In analyzing the resistance on the netting, we also discovered that resistance was increased with increase in the flow velocity and solidity ratio. An analysis of the hydrodynamic coefficient acting on the netting is shown that the drag coefficient tends to increase as the attack angle increases. We also analyzed the hydrodynamic coefficient according to the variation of the Reynolds number. When the drag coefficients acting on the netting were analyzed with the different Reynolds numbers, the Reynolds number increased from over 0.3 m/s to a relative constant. Finally, the copper alloy nettings had a smaller velocity reduction rate when comparing the flow velocity reduction rate between copper alloy nettings and nylon nettings.

단계투기법에 의한 준설점토의 체적비 산정 (Estimation of volume Ratio according to Step up Filling Method for a Dredged Clay)

  • 이송;강명찬
    • 한국지반공학회논문집
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    • 제16권1호
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    • pp.167-178
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    • 2000
  • 준설매립 공사시 자중압밀침하량 및 체적변화비 예측을 위해 사용되는 Yano 방법의 단점을 보완하고실제 준설매립 공사시 준설토가 연속적으로 투기되며 퇴적고의 상승이 토층의 증가와 침강 및 자중압밀에 의한 체적감소의 결과로 표현되어지는 것을 고려한 단계투기법에 의한 새로운 해석기법에 대한 시험적 연구를 수행하였다. 단계투기시험에 의해 투기속도와 퇴적고 상승속도의 관계를 측정하여 현장 매립계획고에 소요되는 현장투기 완료일수를 산정하였고 그때 소요되는 전체 투기높이 그리고 이에 해당하는 실질토량고를 산정하여 이를 바탕으로 현장투기완료 후 자중압밀 침하량 및 체적변화비,함수비, 간극비의 변화를 예측하였고, 전체투기 시험을 통한 Yano법에 의한 산정결과와 비교 분석하였다. 자중압밀 침하량의 경우 약 29.8%, 체적비의 경우 31.1%, 공극비 및 함수비가 약 40%정도 전체투기에 의한 Yano 법이 단계투기법에 의한 결과보다 작게 평가되었다.

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Performance Improvement of Weis-Fogh Type Ship's Propulsion Mechanism Using Spring Type Elastic Wing

  • Ro, Ki-Deok;Cheon, Jung-Hui;Kim, Won-Cheol
    • Journal of Advanced Marine Engineering and Technology
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    • 제33권1호
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    • pp.52-61
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    • 2009
  • This experiment was conducted in attempt of improving hydrodynamic efficiency of the propulsion mechanism by installing a spring to the wing so that the opening angle of the wing in one stroke can be changed automatically, compared to the existing method of fixed maximum opening angle in Weis-Fogh type ship propulsion mechanism. Average thrust coefficient was almost fixed with all velocity ratio with the prototype, but with the spring type, thrust coefficient increased sharply as velocity ratio increased. Average propulsive efficiency was larger with bigger opening angle in the prototype, but in the spring type, the one with smaller spring coefficient had larger value. In the range over 1.0 in velocity ratio where big thrust can be generated, spring type had more than twice of propulsive efficiency increase compared to the prototype.