• 제목/요약/키워드: angle of incidence

검색결과 583건 처리시간 0.029초

하악우각부골절에서 제3대구치의 역할에 관한 통계적 연구 (THE ROLE OF MANDIBULAR THIRD MOLAR IN THE MANDIBULAR ANGLE FRACTURES)

  • 오승환
    • Maxillofacial Plastic and Reconstructive Surgery
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    • 제20권3호
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    • pp.207-213
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    • 1998
  • Purpose : This study attempted to relate the incidence of fractures at the mandibular angle with the presence and state of eruption of lower third molars, and to find out the real risk factors for angle fractures in the states of lower third molars. Materials and Methods : Medical records and radiographs of 395 patients with mandibular fractures were retrospectively reviewed. The presence and states of third molars were assessed for each patients and related to the occurrence of angle and other mandibular fractures. Results : Of 395 patients with mandibular fractures, 142 had angle fractures. The incidence of angle fractures was found to be significantly greater when partial erupted lower third molars were present and it had a definite role for risk factors for angle fractures. But there were no clear relationship between the incidence of angle fracrtures and states of without, fully erupted lower third molars. Furthermore, the states of patial and unerupted lower third molar had an effect on bony segment displacement. Conclusions : This study provides clinical evidence to suggest that patial erupted third molar teeth weaken the mandibular angle both quantitatively and qualitatively.

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A new method to predict the critical incidence angle for buildings under near-fault motions

  • Sebastiani, Paolo E.;Liberatore, Laura;Lucchini, Andrea;Mollaioli, Fabrizio
    • Structural Engineering and Mechanics
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    • 제68권5호
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    • pp.575-589
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    • 2018
  • It is well known that the incidence angle of seismic excitation has an influence on the structural response of buildings, and this effect can be more significant in the case of near-fault signals. However, current seismic codes do not include detailed requirements regarding the direction of application of the seismic action and they have only recently introduced specific provisions about near-fault earthquakes. Thus, engineers have the task of evaluating all the relevant directions or the most critical conditions case by case, in order to avoid underestimating structural demand. To facilitate the identification of the most critical incidence angle, this paper presents a procedure which makes use of a two-degree of freedom model for representing a building. The proposed procedure makes it possible to avoid the extensive computational effort of multiple dynamic analyses with varying angles of incidence of ground motion excitation, which is required if a spatial multi-degree of freedom model is used for representing a building. The procedure is validated through the analysis of two case studies consisting of an eight- and a six-storey reinforced concrete frame building, selected as representative of existing structures located in Italy. A set of 124 near-fault ground motion records oriented along 8 incidence angles, varying from 0 to 180 degrees, with increments of 22.5 degrees, is used to excite the structures. Comparisons between the results obtained with detailed models of the two structures and the proposed procedure are used to show the accuracy of the latter in the prediction of the most critical angle of seismic incidence.

터빈입사각에 따른 회전하는 터빈의 성능에 관한 실험적 연구 (An Experimental Study of the Performance on a Rotating Turbine with Various incidences)

  • 조종현;조수용;조태환
    • 한국항공우주학회지
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    • 제32권9호
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    • pp.94-102
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    • 2004
  • 본 연구에서는 회전하는 터빈에서 입사각을 변경하면서 성능을 측정하여, 최적의 입사각을 찾기 위한 실험적 연구를 수행하였다. 입사각은 터빈 익형의 설계에 중요한 설계변수이기 때문에 최적의 입사각을 찾기 위한 실험적 연구가 많이 수행되었었다. 하지만 대부분의 연구가 직선형이나 환형의 케스케이드에서 수행되었기에 이러한 실험장치에서 얻어진 최적의 입사각을 회전하는 터빈에 적용하는 것은 문제가 없다. 따라서 본 연구에서는 회전하는 터빈에서 입사각의 변경에 다른 성능을 측정하여 최적의 입사각을 얻고자 하였다. 실험결과는 터빈의 성능이 입사각의 변경에 따라 상당한 영향을 받고 있음을 보여주고 있으며 적용 가능한 입사각의 범위는 터빈에 가하여지는 입력공기력의 증가에 따라서 좁아지는 경향을 보여주고 있다. 본 실험에 적용된 익형에서의 최적입사각은 $-12^{\circ}$를 나타내었다.

Computation of Turbulent Flows and Radiated Sound From Axial Compressor Cascade

  • Lee, Seungbae;Kim, Hooi-Joong;Kim, Jin-Hwa;Song, Seung-Jin
    • Journal of Mechanical Science and Technology
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    • 제18권2호
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    • pp.272-285
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    • 2004
  • The losses at off-design points from a compressor cascade occur due to the deviation from a design incidence angle at the inlet of the cascade. The self-noise from the blade cascade at off-design points comes from a separated boundary layer and vortex sheddings. If the incidence angle to the cascade increases, stalling in blades may occur and the noise level increases significantly. This study applied Large-Eddy Simulations (LES) using deductive and deductive dynamic SGS models to low Mach-number, turbulent flow with each incidence angle to the cascade ranging from -40$^{\circ}$ to +20$^{\circ}$ and compared numerical predictions with measured data. It was observed that the oscillating separation bubbles attached to the suction surface do not modify wake flows dynamically for cases of negative incidence angles. However, an incidence angle greater than 8$^{\circ}$ caused a separated vortex near the leading edge to be shed downstream and created stalling. The computed performance parameters such as drag coefficient and total pressure loss coefficient showed good agreement with experimental results. Noise from the cascade of the compressor is summarized as sound generated by a structure interacting with unsteady, turbulent flows. The hybrid method using acoustic analogy was observed to closely predict the measured overall sound powers and directivity patterns at design and off-design points of blade cascade.

Fragility characteristics of skewed concrete bridges accounting for ground motion directionality

  • Jeon, Jong-Su;Choi, Eunsoo;Noh, Myung-Hyun
    • Structural Engineering and Mechanics
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    • 제63권5호
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    • pp.647-657
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    • 2017
  • To achieve this goal, two four-span concrete box-girder bridges with typical configurations of California highway bridges are selected as representative bridges: an integral abutment bridge and a seat-type abutment bridge. A detailed numerical model of the representative bridges is created in OpenSees to perform dynamic analyses. To examine the effect of earthquake incidence angle on the fragility of skewed bridges, the representative bridge models are modified with different skew angles. Dynamic analyses for all bridge models are performed for all earthquake incidence angles examined. Simulated results are used to develop demand models and component and system fragility curves for the skewed bridges. The fragility characteristics are compared with regard to earthquake incidence angle. The results suggest that the earthquake incidence angle more significantly affects the seismic demand and fragilities of the integral abutment bridge than the skewed abutment bridge. Finally, a recommendation to account for the randomness due to the ground motion directionality in the fragility assessment is made in the absence of the predetermined earthquake incidence angle.

스트레이크 붙임각이 이중 삼각날개의 와류에 미치는 영향 (Effects of Strake Incidence-Angle on the Vortex Flow of a Double-Delta Wing)

  • 손명환;정형석;장조원
    • 한국항공우주학회지
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    • 제34권10호
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    • pp.7-15
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    • 2006
  • 스트레이크를 부착한 이중 삼각 날개에서 스트레이크의 붙임각이 날개면 압력분포와 와류 특성에 미치는 영향을 실험적으로 연구하였다. 스트레이크 붙임각의 음(-)방향 증가(스트레이크가 주 날개 윗면으로부터 pitch-down방향으로 부착된 상태)는 날개 전체의 받음각을 증가시키는 것과 같은 효과를 가져와 날개 윗면의 부압의 크기를 증가시켰다. 이러한 스트레이크 붙임각 변화에 의한 날개 윗면 부압 분포 변화는 와류의 강도 변화에 기인하기 보다는 와류 중심이 날개면에 가까이 위치하는 것에 기인하였다.

분광 타원해석기 입사각의 정밀 보정 (Precise calibration of the angle of ncidence in spectroscopic ellipsometer)

  • 김현종;김상열;이윤우;조현모;조용재;이인원
    • 한국광학회지
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    • 제10권3호
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    • pp.208-213
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    • 1999
  • 반도체 및 박막의 두께 측정에 많이 이용되는 분광 타원해석기의 입사각을 정밀하게 보정하기 위한 방법을 제안하고 이를 실험적으로 확인하였다. 몇 종류의 광학유리를 이용하여 프리즘과 기판을 가공하였다. 프리즘의 꼭지각과 최소 벗어나 기각을 측정해 광학유리의 굴절률을 결정하였고 브루스터각(Brewster's angle)에서 측정한 유리기판의 타원해석 스펙트럼을 분석하기 위한 기준값으로 이 굴절률을 사용하여 분광 타원해석기의 입사각을 0.01도의 정밀도로 결정,보정하였다.

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Efficiency of Photovoltaic Cell with Random Textured Anti Glare (RTAG) Glass

  • Kim, Geon Ho;Jeon, Bup Ju
    • Applied Science and Convergence Technology
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    • 제25권6호
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    • pp.133-137
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    • 2016
  • The surface treatment of cover glass for conversion efficiency of photovoltaic cell is important to reduce reflectivity and to increase the incident light. In this work, random textured anti glare (RTAG) glass was prepared by wet surface coating method. Optical properties due to the changes of surface morphology of RTAG glass were compared and conversion efficiency of photovoltaic cell was researched. Grain size and changes of surface morphologies formed with surface etching time greatly affected optical transmittance and transmission haze. Current density (Jsc) were high at the condition when surface morphologies reflection haze were low and transmission haze were high. Jsc was $40.0mA/cm^2$ at glancing angle of $90^{\circ}$. Incidence light source was strongly influenced by surface treatment of cover glass at high incidence angle but was hardly affected light source at the low angle of incidence.

탈설계점에서의 선형 터빈 익열 끝벽 열(물질)전달 특성 (Endwall Heat (Mass) Transfer Characteristics of a Linear Turbine Cascade at Off-Design Conditions)

  • 이상우;박진재
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.1092-1097
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    • 2004
  • The heat (mass) transfer characteristics on the endwall surface of a first-stage linear turbine rotor cascade at off-design conditions has been investigated by employing the naphthalene sublimation technique. The experiments are carried out at the Reynolds number of $2.78{\times}10^{5}$ for two incidence angles of -5% and +5%. The positive incidence angle results in intensification of the pressure-side leg of a leading-edge horseshoe vortex, which delivers higher heat transfer along its trace. On the other hand, the negative incidence angle show an opposite tendency.

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입사각이 터빈 동익 팁누설유동 영역에서의 압력손실에 미치는 영향 (Effects of Incidence on Aerodynamic Losses in the Tip-Leakage Flow Region of a High-Turning Turbine Rotor Blade)

  • 채병주;이상우
    • 한국유체기계학회 논문집
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    • 제13권2호
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    • pp.41-47
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    • 2010
  • The effect of incidence angle on the three-dimensional flow and aerodynamic loss in the tip leakage flow region downstream of a turbine rotor cascade has been investigated for two tip gap-to-chord ratios of h/c=0.0% (no tip gap) and 2.0%. The incidence angle is changed to be $i=-10^{\circ}$, $0^{\circ}$, and $5^{\circ}$. The results show that for $i=5^{\circ}$, secondary flows including the passage vortex are intensified noticeably, and there is a strong interaction between the passage and tip leakage vortices. For $i=-10^{\circ}$, however, the passage vortex is weakened significantly, so that there exists only a strong leakage-jet-like secondary flows near the casing wall. For h/c=0.0% and 2.0%, aerodynamic loss tends to increase with increasing i from $-10^{\circ}$ to $5^{\circ}$. A small increment of i in its positive incidence range results in a remarkable aerodynamic loss increase, while increasing i in the negative incidence range leads to a small change in the aerodynamic loss generation.