• 제목/요약/키워드: Vector Flow

검색결과 675건 처리시간 0.024초

Modeling properties of self-compacting concrete: support vector machines approach

  • Siddique, Rafat;Aggarwal, Paratibha;Aggarwal, Yogesh;Gupta, S.M.
    • Computers and Concrete
    • /
    • 제5권5호
    • /
    • pp.461-473
    • /
    • 2008
  • The paper explores the potential of Support Vector Machines (SVM) approach in predicting 28-day compressive strength and slump flow of self-compacting concrete. Total of 80 data collected from the exiting literature were used in present work. To compare the performance of the technique, prediction was also done using a back propagation neural network model. For this data-set, RBF kernel worked well in comparison to polynomial kernel based support vector machines and provide a root mean square error of 4.688 (MPa) (correlation coefficient=0.942) for 28-day compressive strength prediction and a root mean square error of 7.825 cm (correlation coefficient=0.931) for slump flow. Results obtained for RMSE and correlation coefficient suggested a comparable performance by Support Vector Machine approach to neural network approach for both 28-day compressive strength and slump flow prediction.

Study on the Fluidic Thrust Vector Control Using Co-Flow Concept

  • Wu, Kexin;Jin, Yingzi;Kim, Heuy Dong
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
    • /
    • pp.675-678
    • /
    • 2017
  • In the present, various methods have been employed to obtain the lesser thrust loss. Numerical simulations have been carried out for optimizing the thrust vector control system. Thrust vector control based on coflowing shear layer is an effective method to control the primary jet direction in the absence of moving parts. Thrust vector in symmetric nozzles is acquired by secondary flow injections that result to boundary layer separation. The pressure in secondary flow inlet was varied to check the deflection angle of jet flow.

  • PDF

Snake 모델에서의 개선된 Gradient Vector Flow: 캡쳐 영역의 확장과 요면으로의 빠른 진행 (Enhanced Gradient Vector Flow in the Snake Model: Extension of Capture Range and Fast Progress into Concavity)

  • 조익환;송인찬;오정수;엄경식;김종효;정동석
    • 한국정보과학회논문지:소프트웨어및응용
    • /
    • 제33권1호
    • /
    • pp.95-104
    • /
    • 2006
  • Gradient vector flow(GVF) snake 또는 active contour 모델은 영상 분할에서 훌륭한 성능을 보여준다. 그러나 기존의 snake 모델에는 제한된 캡쳐 영역과 요면으로의 느린 진행과 같은 문제점들이 존재한다. 본 논문은 주변의 필드로부터 외부장(external force field)을 확장시키고 변형된 평탄화기법을 이용하여 확장된 필드를 정규화 함으로서 GVF snake 모델의 성능을 개선시키는 새로운 방법을 제시한다. 시뮬레이션을 위해 사용된 U자 모양 이미지에서의 결과는 제안된 방법이 좀 더 큰 캡쳐 영역을 갖고 기존의 GVF snake 모델에 비하여 요면으로 빠르게 진행하는 것이 가능함을 보여준다.

Augmenting Quasi-Tree Search Algorithm for Maximum Homogenous Information Flow with Single Source/Multiple Sinks

  • Fujita, Koichi;Watanabe, Hitoshi
    • 대한전자공학회:학술대회논문집
    • /
    • 대한전자공학회 2002년도 ITC-CSCC -1
    • /
    • pp.462-465
    • /
    • 2002
  • This paper presents a basic theory of information flow from single sending point to multiple receiving points, where new theories of algebraic system called "Hybrid Vector Space" and flow vector space play important roles. Based on the theory, a new algorithm for finding maximum homogenous information flow is proposed, where homogenous information flow means the flow of the same contents of information delivered to multiple clients at a time. Effective multi-routing algorithms fur tree-shape delivery rout search are presented.

  • PDF

2차 유동 분사를 이용한 추력벡터 제어에 관한 수치해석적 연구 (A Computational Study of the Fluidic Thrust Vector Control Using Secondary Flow Injection)

  • 임채민;김희동
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2003년도 추계학술대회
    • /
    • pp.496-501
    • /
    • 2003
  • Computational study is performed to understand the fluidic thrust vectoring control of an axisymmetric nozzle, in which secondary gas injection is made in the divergent section of the nozzle. The nozzle has a design Mach number of 2.0, and the operation pressure ratio is varied to obtain the different flow features in the nozzle flow. The injection flow rate is varied by means of the injection port pressure. Test conditions are in the range of the nozzle pressure ratio from 3.0 to 8.26 and the injection pressure ratio from 0 to 1.0. The present computational results show that, for a given nozzle pressure ratio, an increase of the injection pressure ratio produces increased thrust vector angle, but decreases the thrust efficiency.

  • PDF

Velocity Field Masking Technique for Coastal Engineering Experiments

  • Adibhusana, Made Narayana;Ryu, Yong-Uk
    • 한국수자원학회:학술대회논문집
    • /
    • 한국수자원학회 2021년도 학술발표회
    • /
    • pp.154-154
    • /
    • 2021
  • Since the development of Bubble Image Velocimetry (BIV) technique as the complementary technique of Particle Image Velocimetry (PIV), the application of digital imaging technique in the field of hydraulic and coastal engineering increased rapidly. BIV works very well in multi-phase flow (air-water) flows where the PIV technique doesn't. However, the velocity field obtained from BIV technique often resulted in a velocity vector on the outside of the flow (false velocity) since the Field of View (FOV) usually not only cover the air-water flow but also the area outside the flow. In this study, a simple technique of post processing velocity field was developed. This technique works based on the average of the pixel value in the interrogation area. An image of multi-phase flow of wave overtopping was obtained through physical experiment using BIV technique. The velocity calculation was performed based on the similar method in PIV. A velocity masking technique developed in this study then applied to remove the false velocity vector. Result from non-masking, manually removed and auto removed false velocity vector were presented. The masking technique show a similar result as manually removed velocity vector. This method could apply in a large number of velocity field which is could increase the velocity map post-processing time.

  • PDF

Coflow-Counterflow 개념을 이용한 추력벡터 노즐에서 발생하는 유동특성에 관한 연구 (A Study of Thrust-Vectoring Nozzle Flow Using Coflow-Counterflow Concept)

  • 정성재;;김희동
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2003년도 추계학술대회
    • /
    • pp.592-597
    • /
    • 2003
  • Thrust vector control using a coflow-counterflow concept is achieved by suction and blowing through a slot adjacent to a primary jet which is shrouded by a suction collar. In the present study, the flow characteristics of thrust vectoring is investigated using a numerical method. The nozzle has a design Mach number of 2.0, and the operation pressure ratio is varied to obtain various flow features of the nozzle flow. Test conditions are in the range of the nozzle pressure ratio from 6.0 to 10.0, and a suction pressure from 90kPa to 35kPa. Two-dimensional, compressible Navier-Stokes computations are conducted with RNG ${\kappa}-{\varepsilon}$ turbulence model. The computational results provide an understanding of the detailed physics of the thrust vectoring process. It is found that an increase in the nozzle pressure ratio leads to increased thrust efficiency but reduces the thrust vector angle.

  • PDF

H.264에서 에러은닉을 위한 OPtical Flow기반의 움직임벡터 복원 기법 (A Motion Vector Recovery Method based on Optical Flow for Temporal Error Concealment in the H.264 Standard)

  • 김동형;정제창
    • 한국통신학회논문지
    • /
    • 제31권2C호
    • /
    • pp.148-155
    • /
    • 2006
  • H.264/AVC 부호화 표준은 이전의 여러 부호화 표준에는 없던 새로운 부호화 도구들이 추가되었으며 이를 통해 보다 높은 압축 효율을 가진다. 추가된 여러 부호화 도구들 중 최소 4$\times$4 단위의 움직임 추정은 이전보다 인접한 블록들 사이의 움직임벡터 상관도를 높이는 결과를 가져오며, 이러한 특징은 움직임벡터 복원을 통한 에러은닉 기법에 효율적으로 사용될 수 있다. 본 논문은 옵티컬 플로워에 기반하여 움직임 벡터를 복원하는 에러은닉 방법을 제안한다. 인접한 매크로블록들 사이의 움직임벡터들 사이의 상관도가 이전의 여러 부호화 표준들에 비하여 높은 H.264 부호화 표준의 특징을 이용하여 제안하는 알고리듬은 비교적 정확한 초기값의 설정과 속도벡터를 구하기 위한 영역을 16$\times$16크기로 제한함으로써 복잡도를 경감시킨다. 실험결과 제안하는 알고리듬은 다양한 비트율 및 다양한 매크로블록 오류율에서 이전 동일 블록 복사를 수행하는 시방향 복사 방법뿐만 아니라 JM10.1에 구현되어 있는 에러은닉 기법보다 주관적 및 객관적 화질이 높은 것으로 나타난다.

2차 유동 분사에 의한 제트 유동의 추력 제어에 관한 연구 (Study of the Thrust Vector Control using a Secondary Flow Injection)

  • 정성재;;김희동;안재문;정동호
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2002년도 학술대회지
    • /
    • pp.119-122
    • /
    • 2002
  • In general, Liquid Injection Thrust Vector Control(LITVC) is accomplished by injecting a liquid into the supersonic exhaust flow through holes in the wall of the propulsion nozzle. This injection flow field is highly complicated and detailed flow physics associated with the secondary flow injection should be known far the practical design and use of the LITVC system. The present study aims at understanding the LTTVC flow field and obtaining fundamental design parameters for LITVC. The experimentations were performed in a supersonic blow-down wind tunnel. Compressed, dry air was used for both the main exhaust and injection flows but the pressures of these two flows were controlled independently. The location of the injection holes was changed and the pressures of the two streams were also changed between 2.0 and 15.0 bar. The effectiveness of LITVC was discussed in details using the results of the pressure measurements and flow visualizations

  • PDF

속도 벡터 영상 방법 (Velocity Vector Imaging)

  • 권성재
    • The Journal of the Acoustical Society of Korea
    • /
    • 제29권1E호
    • /
    • pp.11-27
    • /
    • 2010
  • Nowadays, ultrasound Doppler imaging is widely used in assessing cardiovascular functions in the human body. However, a major drawback of ultrasonic Doppler methods is that they can provide information on blood flow velocity along the ultrasound beam propagation direction only. Thus, the blood flow velocity is estimated differently depending on the angle between the ultrasound beam and the flow direction. In order to overcome this limitation, there have been many researches devoted to estimating both axial and lateral velocities. The purpose of this article is to survey various two-dimensional velocity estimation methods in the context of Doppler imaging. Some velocity vector estimation methods can also be applied to determine tissue motion as required in elastography. The discussion is mainly concerned with the case of estimating a two-dimensional in-plane velocity vector involving the axial and lateral directions.