• Title/Summary/Keyword: 3 dimensional configuration

Search Result 339, Processing Time 0.025 seconds

Comparisons of 2-D and 3-D IVR experiments for oxide layer in the three-layer configuration

  • Bae, Ji-Won;Chung, Bum-Jin
    • Nuclear Engineering and Technology
    • /
    • v.52 no.11
    • /
    • pp.2499-2510
    • /
    • 2020
  • We performed 3-D (3-dimensional) IVR (In-Vessel Retention) natural convection experiments simulating the oxide layer in the three-layer configuration, varying the aspect ratio (H/R). Mass transfer experiment was conducted based on the analogy to achieve high RaH's of 1.99 × 1012-6.90 × 1013 with compact facilities. Comparisons with 2-D (2-dimensional) experiments revealed different local heat transfer characteristics on upper and lower boundaries of the oxide layer depending on the H/R. For the 3-D shallow oxide layer, the multi-cell flow patterns appeared and the number of cells was considerably increased with the H/R decreases, which differs with the 2-D experiments that the number of cells was independent on H/R. Thus, the enhancement of the downward heat transfer and the mitigation of the focusing effect were more noticeable in the 3-D experiments.

A TWO-DIMENSIONAL CFD MODEL OF SMALL TURBOJET COMBUSTOR (소형 터보제트엔진 연소기의 2차원 전산유체해석 모델)

  • Lee, Se-Min;Park, Soo-Hyung;Lee, Chang-Jin;Lee, Dong-Hun;Paeng, Ki-Seok;Ryu, Jong-Hyeok;Ryu, Kyung-Won
    • 한국전산유체공학회:학술대회논문집
    • /
    • 2008.03a
    • /
    • pp.155-158
    • /
    • 2008
  • A practical modeling approach of a small slinger combustor is proposed and a 2-dimensional axisymmetric computational model is developed. Based on numerical results from the full 3-dimensional configuration, model reduction is achieved toward 2-dimensional axisymmetric configuration. By simplifying the complex model, computing time can be significantly reduced and it makes easy to find effects of geometry modification. Numerical results show that the flow characteristic of 2-D model is quite similar to that of the 3-D configuration.

  • PDF

Use of cone-beam computed tomography and three-dimensional modeling for assessment of anomalous pulp canal configuration: a case report

  • Sinanoglu, Alper;Helvacioglu-Yigit, Dilek;Mutlu, Ibrahim
    • Restorative Dentistry and Endodontics
    • /
    • v.40 no.2
    • /
    • pp.161-165
    • /
    • 2015
  • Three-dimensional (3D) reconstruction of cone-beam computed tomography (CBCT) scans appears to be a valuable method for assessing pulp canal configuration. The aim of this report is to describe endodontic treatment of a mandibular second premolar with aberrant pulp canal morphology detected by CBCT and confirmed by 3D modeling. An accessory canal was suspected during endodontic treatment of the mandibular left second premolar in a 21 year old woman with a chief complaint of pulsating pain. Axial cross-sectional CBCT scans revealed that the pulp canal divided into mesiobuccal, lingual, and buccal canals in the middle third and ended as four separate foramina. 3D modeling confirmed the anomalous configuration of the fused root with a deep lingual groove. Endodontic treatment of the tooth was completed in two appointments. The root canals were obturated using lateral compaction of gutta-percha and root canal sealer. The tooth remained asymptomatic and did not develop periapical pathology until 12 months postoperatively. CBCT and 3D modeling enable preoperative evaluation of aberrant root canal systems and facilitate endodontic treatment.

Wing Design Optimization of a Solar-HALE Aircraft

  • Lim, JaeHoon;Choi, Sun;Shin, SangJoon;Lee, Dong-Ho
    • International Journal of Aeronautical and Space Sciences
    • /
    • v.15 no.3
    • /
    • pp.219-231
    • /
    • 2014
  • We develop a preliminary design optimization procedure in this paper regarding the wing planform in a solar-powered high-altitude long-endurance unmanned aerial vehicle. A high-aspect-ratio wing has been widely adopted in this type of a vehicle, due to both the high lift-to-drag ratio and lightweight design. In the preliminary design, its characteristics need to be addressed correctly, and analyzed in an appropriate manner. In this paper, we use the three-dimensional Euler equation to analyze the wing aerodynamics. We also use an advanced structural modeling approach based on a geometrically exact one-dimensional beam analysis. Regarding the structural integrity of the wing, we determine detailed configuration parameters, specifically the taper ratio and the span length. Next, we conduct a multi-objective optimization scheme based on the response surface method, using the present baseline configuration. We consider the structural integrity as one of the constraints. We reduce the wing weight by approximately 25.3 % from that in the baseline configuration, and also decrease the power required approximately 3.4 %. We confirm that the optimized wing has sufficient flutter margin and improved static longitudinal/directional stability characteristics, as compared to those of the baseline configuration.

Optimization of Flap Shape and Position for Two-dimensional High Lift Device (2차원 고양력장치의 플랩 형상 및 위치 최적화)

  • Park, Youngmin;Kang, Hyoungmin;Chung, Jindeog;Lee, Hae-Chang
    • Journal of Aerospace System Engineering
    • /
    • v.7 no.3
    • /
    • pp.1-6
    • /
    • 2013
  • Numerical optimization of two dimensional high lift configuration was performed with flow solver and optimization method based on RSM(Response Surface Model). Navier-Stokes solver with Spalart-Allmaras turbulence model was selected for the simulation of highly complex and separated flows on the flap. For the simultaneous optimization of both flap shape and setting (gap/overlap), 10 design variables (eight variables for flap shape variation and two variables for flap setting) were chosen. In order to generate the response surface model, 128 experimental points were selected for 10 design variables. The objective function considering maximum lift coefficient, lift to drag ratio and lift coefficient at specific angle of attack was selected to reduce flow separation on the flap surface. The present method was applied to two dimensional fowler flap in landing configuration. After applying the present method, it was shown that the optimized high lift configuration had less flow separation on the flap surface and lift to drag ratio was suppressed over entire angle of attack range.

A Method for Constructing 3-Dimensional C-obstacles Using Free Arc (프리아크를 이용한3차원 형상 공간 장애물 구성 방법)

  • 이석원;임충혁
    • Journal of Institute of Control, Robotics and Systems
    • /
    • v.8 no.11
    • /
    • pp.970-975
    • /
    • 2002
  • We suggests an effective method to construct time-varying C-obstacles in the 3-dimensional configuration space (C-space) using free arc. The concept of free arc was defined mathematically and the procedure to find free arc in the case off-dimensional C-space was derived in [1]. We showed that time-varying C-obstacles can be constructed efficiently using this concept, and presented simulation results for two SCARA robot manipulators to verify the efficacy of the proposed approach. In this paper, extensions of this approach to the 3-dimensional C-space is introduced since nearly all industrial manipulators are reasonably treated ill the too or three dimensional C-space f3r collision avoidance problem The free arc concept is summarized briefly and the method to find lice arc in the 3-dimensional f-space is explained. To show that this approach enables us to solve a practical collision avoidance problem simulation results f3r two PUMA robot manipulators are presented.

A Study on the Prediction of Bone Remodeling of Plated-Human Femur using 3-Dimensional Finite Element Method (3차원 유한요소법을 이용한 골절판에 대한 인체 대퇴골의 골재형성에 관한 연구)

  • 김현수
    • Journal of Biomedical Engineering Research
    • /
    • v.13 no.4
    • /
    • pp.353-362
    • /
    • 1992
  • The stress distribution of bone is altered by the rigid bone plate, sometimes resulting in unfavorable osteoporosis. The rigidity and the biocompatibility are important factors for the design of prosthesis. However, it is also necessary to consider the effect on the bone remodeling. In this paper, it is attempted to establish an approximate and simple method to predict the trend of the configuration of surface bone remodeling for the case of a bone plate using stress analysis. Thus, three dimensional finite element model of plated-human femur is generated and simulated. In addition. the stress difference method (SDM) is introduced and attempted to demonstrate the configuration of surface bone remodeling of the plated-human femur. The results are compared with those of invivo tests and the feasibility of the stress difference method is discussed.

  • PDF

A Study on the 3D Scanning of Fashionable Textile Materials - Ripple-finished Cotton Fabric and Shrink-proof Finished/Felted Wool Fabric -

  • Kim, Jong-Jun
    • Journal of Fashion Business
    • /
    • v.15 no.6
    • /
    • pp.101-112
    • /
    • 2011
  • Three-dimensional(3D) virtual clothing simulation system may require the use of physical, mechanical, and configurational data in order to mimic the actual clothing with high degree of realism. Therefore the 3-dimensional scanning system based on optical methods was adopted to extract the 3-dimensional data of the fabric surface. In this study, the appearances of the 3-dimensionally transformed textile fabrics via several finishing procedures were investigated using a 3D scanning system. The wool gauze fabrics treated with the shrink-proof finishing and the felting process showed height changes up to 4.5mm. The 3-dimensional configuration may be objectively described by the use of mesh generation from the scanned output. The generated mesh information may further be utilized in the 3D virtual clothing simulation system for accurate description of the fashionable textile materials used in the simulation system.

The Effects of Three Dimensional Stimulus Configuration on Self-Motion Perception Induced by Large Visual Display

  • Nakamura, Shinji
    • 한국정보디스플레이학회:학술대회논문집
    • /
    • 2007.08a
    • /
    • pp.1031-1034
    • /
    • 2007
  • The interactions between two-dimensional and three-dimensional stimulus configurations on visually induced self-motion perception (vection) were examined. The experiment revealed that there is no 2D-3D interaction, and vection strength is determined solely by the size of the moving background stimulus, which should be a primary factor in inducing vection.

  • PDF

Dynamic response of pile groups in series and parallel configuration

  • Sawant, V.A.;Ladhane, K.B.
    • Structural Engineering and Mechanics
    • /
    • v.41 no.3
    • /
    • pp.395-406
    • /
    • 2012
  • Basic problem of pile foundation is three dimensional in nature. Three dimensional finite element formulation is employed for the analysis of pile groups. Pile, pile-cap and soil are modeled using 20 node element, whereas interface between pile or pile cap and soil is modeled using 16 node surface element. A parametric study is carried out to consider the effect of pile spacing, number of piles, arrangement of pile and soil modulus on the response of pile group. Results indicate that the response of pile group is dependent on these parameters.