• 제목/요약/키워드: Drop simulations

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Numerical study on the design of urea decomposition chamber in LP SCR system

  • Um, Hyung Sik;Kim, Daehee;Kim, Keon Ho
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.11 no.1
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    • pp.307-313
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    • 2019
  • In order to design efficient Urea Decomposition Chamber (UDC) for the Low Pressure (LP) Selective Catalytic Reduction (SCR) system, numerical simulations were conducted with respect to various design parameters. The design parameters examined in this simulation include the chamber diameter, inlet and outlet shape of chamber, and urea injection point. Reaction kinetics for the urea decomposition was proposed and validated with the experimental data in the range of $300{\sim}450^{\circ}C$. The effects of design parameters on the performance of UDC were evaluated by the calculated urea conversion and pressure drop. As a result, the local optimum design values were derived by the parametric study.

Numerical Simulation of Air Flows in Human Upper Airway for Free Flap Reconstruction Following Resection Surgery in Oral Cancer Patients (구강암 절제 및 재건 수술에 따른 기도 내 공기 유동 시뮬레이션)

  • Seo, Heerim;Song, Jae Min;Yeom, Eunseop
    • Journal of the Korean Society of Visualization
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    • v.18 no.3
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    • pp.96-102
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    • 2020
  • Oral cancer surgery changes the morphologic characteristics of the human upper airway. These changes can affect the flow patterns. In this study, computational fluid dynamics (CFD) simulations with transient solver were performed to numerically investigate the air flows in the human upper airways depending oral cancer surgery. 3D reconstructed models were obtained from 2D CT images of one patient. For the boundary condition, the realistic breathing cycle of human was applied. The hydraulic diameters of cross-sections for post-surgical model are changed greatly along streamwise direction, so these variations can cause higher wall shear stress and flow disturbance compared to pre-surgical model. The recirculation flows observed in the protruding region result in the relatively large pressure drop. These results can be helpful to understand the flow variations after resection surgery of oral cancer.

Flow Characteristics of Upper Airway After Neck Dissection and Reconstructive Surgery in Tongue Cancer Patients (설암 환자에서 경부청소술 및 재건술에 따른 수술 전 후 기도 내 공기 유동 특성)

  • Jae Min Song;Heerim Seo;Eunseop Yeom
    • Journal of the Korean Society of Visualization
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    • v.22 no.2
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    • pp.90-95
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    • 2024
  • This study examined changes in airway airflow characteristics before and after extensive surgery for tongue cancer, which includes neck dissection and reconstruction. Pre- and post-operative CBCT scans were used to model 3D upper airways. Computational fluid dynamics (CFD) simulations analyzed airflow and pressure variations. Results showed a significant reduction in airway volume post-surgery, especially in the posterior tongue and epiglottis areas, leading to increased airflow velocity and complex vortex formations. Pressure drop analysis revealed that post-surgery, higher negative pressure is required for inhalation, indicating increased breathing effort. This suggests that the surgical removal of cancerous tissues and lymph nodes, along with reconstruction, alters airway geometry significantly, potentially impacting respiratory function. The findings highlight the clinical importance of assessing airway changes in tongue cancer surgery to anticipate and mitigate postoperative respiratory complications.

Deriving the Rate Constants of Coal Char-CO2 Gasification using Pressurized Drop Tube Furnace (가압 DTF를 이용한 석탄 촤-CO2 가스화 반응상수 도출)

  • Sohn, Geun;Ye, Insoo;Ra, Howon;Yoon, Sungmin;Ryu, Changkook
    • Journal of the Korean Society of Combustion
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    • v.22 no.4
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    • pp.19-26
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    • 2017
  • This study investigates the gasification of coal char by $CO_2$ under high pressures in a drop tube furnace(DTF). The rate constants are derived for the shrinking core model using the conventional method based on the set reactor conditions. The computational fluid dynamic(CFD) simulations adopting the rate constants revealed that the carbon conversion was much slower than the experimental results, especially under high temperature and high partial pressure of reactants. Three reasons were identified for the discrepancy: i) shorter reaction time because of the entry region for heating, ii) lower particle temperature by the endothermic reaction, and iii) lower partial pressure of $CO_2$ by its consumption. Therefore, the rate constants were corrected based on the actual reaction conditions of the char. The CFD results updated using the corrected rate constants well matched with the measured values. Such correction of reaction conditions in a DTF is essential in deriving rate constants for any char conversion models by $H_2O$ and $O_2$ as well as $CO_2$.

A Study of Core-Stateless Mechanism for Fair Bandwidth Allocation (대역 공평성 보장을 위한 Core-Stateless 기법 연구)

  • Kim, Hwa-Suk;Kim, Sang-Ha;Kim, Young-Bu
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.28 no.4C
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    • pp.343-355
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    • 2003
  • Fair bandwidth allocations at routers protect adaptive flows from non-adaptive ones and may simplify end-to end congestion control. However, traditional fair bandwidth allocation mechanisms, like Weighted Fair Queueing and Flow Random Early Drop, maintain state, manage buffera and perform packet scheduling on a per-flow basis. These mechanisms are more complex and less scalable than simple FIFO queueing when they are used in the interi or of a high-speed network. Recently, to overcome the implementation complexity problem and address the scalability and robustness, several fair bandwidth allocation mechanisms without per-flow state in the interior routers are proposed. Core-Stateless Fair Queueing and Rainbow Fair Queuing are approximates fair queueing in the core-stateless networks. In this paper, we proposed simple Layered Fair Queueing (SLFQ), another core-stateless mechanism to approximate fair bandwidth allocation without per-flow state. SLFQ use simple layered scheme for packet labeling and has simpler packet dropping algorithm than other core-stateless fair bandwidth allocation mechanisms. We presente simulations and evaluated the performance of SLFQ in comparison to other schemes. We also discussed other are as to which SLFQ is applicable.

Active Buffer Management Algorithm for Voice Communication System with Silence Suppression (무음 압축을 이용하는 음성 통신 시스템을 위한 동적 버퍼 관리 알고리즘)

  • Lee, Sung-Hyung;Lee, Hyun-Jin;Kim, Jae-Hyun;Lee, Hyung-Joo;Hoh, Mi-Jeong;Choi, Jeung-Won;Shin, Sang-Heon;Kim, Tae-Wan
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.37 no.7B
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    • pp.528-535
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    • 2012
  • This paper proposes silence drop first(SDF) active buffer management algorithm to increase the voice capacity when silence suppression is used. This algorithm finds and drops silence packet rather than voice packet in the queue for resolving buffer overflow of queue. Simulations with voice codec of G.729A and G.711 are performed. By using proposed SDF algorithm, the voice capacity is increased by 84.21% with G.729A and 38.46% with G.711. Further more, SDF algorithm reduces the required link capacity and loosens the silence packet inter-arrival time limit to provide target voice quality compared with that of conventional algorithms.

Numerical and Experimental Investigation on Impact Performance of Fiber Metal Laminates Based on Thermoplastic Composites (열가소성 복합재료를 기반한 섬유금속적층판의 충격 거동에 관한 실험 및 수치적 연구)

  • Lee, Byoung-Eon;Kang, Dong-Sik;Park, Eu-Tteum;Kim, Jeong;Kang, Beom-Soo;Song, Woo-Jin
    • Transactions of the Korean Society of Automotive Engineers
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    • v.24 no.5
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    • pp.566-574
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    • 2016
  • Fiber metal laminates, which are hybrid materials consisting of metal sheets and composite layers, have contributed to aerospace and automotive industries due to their reduced weight and improved damage tolerance characteristics. In this study, the impact performance of the laminates, which are comprised of a self-reinforced polypropylene and two aluminum sheets, and the pure aluminum alloy sheet material were investigated experimentally via numerical simulation. In order to compare the impact performance, the laminates and aluminum alloy were examined by assessing the impact force, energy time histories, and specific energy absorption. ABAQUS is a commercial software that is used to simulate the actual drop-weight tests. Based on this study, it is noted that the impact performance of the laminates was superior to that of the aluminum alloy. In addition, a good agreement between the experimental and numerical results can be achieved when the impact force and energy time histories from the experiments and the numerical simulations are compared.

Study on Crashworthiness of Icebreaker Steel: Part II Ship Side Structural Behavior Due to Impact Bending (쇄빙선의 내충격 특성에 관한 실험적 연구: 제2부 선체 구조의 충격 굽힘 특성)

  • Noh, Myung-Hyun;Lee, Jae-Yik;Han, Donghwa;Choung, Joonmo
    • Journal of Ocean Engineering and Technology
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    • v.30 no.4
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    • pp.277-286
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    • 2016
  • The first part of this study found the tendencies of the mechanical properties of two arctic structural steels (EH32 and FH32). In the second part, the crashworthiness of stiffened panels scaled down from the side frame structure of a Korean research icebreaker was determined. A procedure for designing the shapes and sizes of the stiffened panels, mass and shape of a drop striker, and a large temperature chamber, and then manufacturing these, is introduced in detail. From impact bending tests for the stiffened panels, the residual permanent deformations and deformation histories over time were captured using manual measurement and video image analyses. Numerical simulations of the impact bending tests were carried out for three different finite element models, which were mainly composed of shell elements, solid elements, and solid elements, with welding beads. It was proven from a comparison of the test results and numerical simulation results that the solid element model with the welding bead consideration approached the test results in terms of the residual deformations as long as the strain rate effect was taken into account.

Numerical Modeling of Wave-Type Flow on a Stepped Weir (계산형 위어에서의 파형흐름 수치모의)

  • Paik, Joongcheol;Kang, Joon Gu;Lee, Nam-Ju
    • Proceedings of the Korea Water Resources Association Conference
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    • 2016.05a
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    • pp.65-65
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    • 2016
  • Various types of flow conditions are developed in the region just downstream of hydraulic structures such as weir and drop structures. One of distinct flow conditions occurred downstream of drop structures is the wave type flow with undular hydraulic jump formation. We present three-dimensional numerical simulations of a wave type flow formed downstream of a stepped weir which were experimentally investigated by Kang et al. (2010). The turbulent flow over the weir structure is modeling using the unsteady Reynolds-averaged Navier-Stokes (URANS) simulation employing the Spalart-Allmaras one equation model and the detached eddy simulation. Numerical modeling and the performance of turbulence modeling approaches are evaluated by comparing with the experimental measurements in terms of the free surface variation, the shapes and sizes of undular wave, roller near at free surface, recirculation zone near the channel bottom downstream of the structures, and streamwise velocity profiles at selected longitudinal locations.

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Hybrid Control of Aircraft Landing Gear using Magnetorheological Damper (MR댐퍼를 적용한 항공기 착륙장치의 하이브리드 제어기법 연구)

  • Tak, Jun Mo;Viet, Luong Quoc;Hwang, Jai-Hyuk
    • Journal of Aerospace System Engineering
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    • v.12 no.1
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    • pp.1-9
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    • 2018
  • In this study, a hybrid control method that adjusts for the existing force control technique has been presented for consideration. The proposed hybrid control technique does away with the chattering phenomenon occurring in existing force control technique and provides high shock absorption efficiency. In order to design the controller for the landing gear with MR damper, the equation of motion of the landing gear was derived. The hybrid controller was designed after constructing a simulation model using Recur-Dyne, multi-body dynamic analysis software. The hybrid controller can reduce the maximum strut force and displacement based on the skyhook controller, and is able to get the high efficiency by making it work for the additional force control technique. In addition, an effective switching control technique and input shaping technique was applied to prevent the chattering in the drop simulation. Finally, the performance of the landing characteristics was evaluated throughout the various drop simulations.