• 항공우주시스템공학회지
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• 제13권5호
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• pp.39-48
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• 2019

회전-고정자 혼합기 내의 난류 유동은 고속으로 회전하는 회전자와 고정자의 상호작용에 의해 발생되는 전단특성을 기반으로 한다. 본 연구에서는 유화연료 관련 회전-고정자 혼합기 시제품 모델에서 회전자와 고정자간의 상호작용에 의한 비정상상태 유동 특성 분석을 ANSYS FLUENT $k-{\varepsilon}$ (RKE) 난류 모델을 MRF 및 SMM에 적용하여 수행하였다. 회전자와 고정자의 경계에서 발생하는 유동 입자들의 거동과 전단 특성 그리고 설계 파라미터에 따른 속도분포와 난류와류소산 등의 경향을 전산유체역학 해석을 통해 예측 비교하여 모델의 효율성을 검증하였다.

• 항공우주시스템공학회지
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• 제15권2호
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• pp.26-35
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• 2021

In this study, CFD analysis was conducted to compare the aerodynamic performance of the isolated propeller and pusher propeller, which is affected by the wake of wide fuselage. The moving reference frame (MRF) method was used for isolated propeller analysis, while the MRF and sliding mesh method were used sequentially for the pusher propeller to analyze the change in the aerodynamic characteristics based on the azimuth angle. Under the same torque condition, the thrust of the pusher propeller was greater than that of the isolated propeller. Thrust increment of the pusher propeller was mainly generated near the root of the blade where the fuselage wake was concentrated. The net efficiency of the pusher propeller was greater than or equal to that of the isolated propeller. Because of the flat fuselage shape, thrust and torque of the pusher propeller periodically changed with the rotation of the propeller.

• International Journal of Naval Architecture and Ocean Engineering
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• 제12권1호
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• pp.918-927
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• 2020

Flows induced by hybrid CRP pod propulsion systems (CRP-POD) are fundamentally characterized by unsteadiness. This work presents a numerical study on the unsteady flow of a CRP-POD at behind-hull condition based on CFD (Computational Fluid Dynamics). Unsteady RANS method is adopted, coupled with SST k-u turbulence model and sliding mesh method. The propeller thrusts and torques obtained by CFD is validated by model tests and acceptable agreements are obtained. The time histories of shingle-blade loads and pressures near the hull surface are recorded for the analysis of unsteady flow features. The cases of forward propeller alone and aft propeller alone are also computed to distinguish the hull-propeller interaction and propeller-propeller interaction. The results show the blade loads of both forward and aft propellers strongly fluctuate with phase angles. For the forward propeller, the blade load fluctuation is mainly governed by the hull-propeller interaction, while the aft blade load is remarkably affected by the propeller-propeller interaction in terms of the load average and fluctuation pattern. The fields of pressure, vorticity and velocity are also analyzed to reveal the unsteady flow features.

• 열처리공학회지
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• 제36권3호
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• pp.137-144
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• 2023

Micro electro mechanical systems (MEMS) and precision machines require excellent friction and wear characteristics to improve energy efficiency generated during sliding motion. In this study, DLC thin film with high hardness and low friction was deposited on STS304 substrate material by CVD method, and dot-shaped convex and concave micropatterns were fabricated by photolithography process. The diameter of the pattern was 20 ㎛, the pitch was 40 ㎛, and a pattern having a mesh type arrangement was fabricated and an abrasion test was performed. The results of the wear test on the micro pattern confirmed that the friction coefficient characteristics were improved compared to STS 304 and DLC thin films. In addition, in this result, the micro-pattern showed 11.4% more improved friction coefficient than the DLC thin film. The friction coefficient characteristics for convex and concave patterns of the same size showed almost similar results.

• 대한조선학회논문집
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• 제60권5호
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• pp.296-304
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• 2023

Cavitation tests for a waterjet propulsor of an amphibious vehicle are carried out in the Large Cavitation Tunnel. Waterjet pump performances and cavitation characteristics including thrust breakdown performances are investigated in the tests. In addition, cavitation characteristics for waterjet propulsors working inside the intake are calculated by using a commercial CFD code, Star-CCM+. Sliding mesh is implemented to a rotating impeller and the k-epsilon turbulence model is chosen. Cavitation bubble growth and collapse are estimated using the Schnerr-Sauer cavitation model based on Rayleigh-Plasset equation. Calculated results agree fairly well with experimental results. The re-design of the waterjet propulsor is performed to enhance waterjet cavitating performances and calculated results show that waterjet thrust breakdown characteristics are significantly improved.

• Applied Microscopy
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• 제10권1_2호
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• pp.7-17
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• 1980

Electron microscope radioautography introduced by Liquier-Milward (1956) is now used routinely in many laboratories. Most of the technical difficulties in specimen preparation have been overcome. This method is modified from loop method for improvement of EM radioautographic techniques. The advantages of this method are: 1. the use of single specimens on small corks and of a large wire loop, allows the experimenter to avoid the blemishes in the membrane; 2. the surfactant dioctyl sodium sulphosuccinate is added to diluted ILford L4, thus greatly prolonging the period of time over which good emulsion layers can be made; 3. corks can be handled in perspex holder which allows about 20 specimens to be developed simultaneously. The steps of the method comprise: 1. Cut ribbons of ultrathin sections of silver interference colour 2. Pick them up on formvar-coated 200 mesh grids 3. Prestaining of tissues 4. Coat the specimens with a thin layer of carbon by evaporation (30-60A) 5. Mount the specimens on corks (about 1cm apical diameter) using double-sided scotch tape 6. Emulsion coating; a. Take a 250m1 beaker, place it on the pan of a sliding weight balance and weigh it. Add 10 grams extra to the beam. Add pieces of ILford L4 emulsion to the beaker until the balance is swinging freely. Add the 20ml of distilled water that was previously measured out. b. Surfactant dioctyl sodium sulphosuccinate is added to diluted ILford L4. 7. Prepare a series of membranes of gelled emulsion with the wire loop and apply one to each cork-borne specimen. 8. Put the specimens away to expose by pushing the corks into short length of PVC tubing, each tube having a small hole in the side 9. Place the tubes in small boxes together with silica gel. 10. Exposure 11. Developer - Kodak Microdol X for 3 minutes 12. Fixer - A perspex holder can be manufactured which allows 20 specimens to be developed simultaneously. 12. Fixer - 30% sodium thiosulfate for 10 minutes 13. Examination with Siemens Elmiskop 1A electron microscope

• 항공우주기술
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• 제11권2호
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• pp.65-72
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• 2012

프로펠러와 고양력장치를 장착한 터보프롭 항공기에 대한 실속 특성 분석을 위해 수치 해석을 수행하였다. 항공기의 실속 특성은 프로펠러와 고양력 장치의 장착 조합에 따른 형상별 전산해석 결과를 통해 정성적으로 분석하였다. 실속 특성 해석은 Spalart-Allmaras 난류 모델을 기반으로 한 3차원 Navier-Stokes 방정식 해법을 이용하였으며 프로펠러의 회전은 슬라이딩 격자기법을 이용하여 모사하였다. 분석 결과 순항 형상의 경우 동체/날개 페어링에서 주요 유동박리가 발생하며 프로펠러 후류로 인해 점차 감소함을 알 수 있었다. 고양력장치를 장착한 경우 나셀 바깥쪽에서 주요 유동박리 현상이 발생하였고 프로펠러가 회전하는 경우에도 상대속도 감소와 유효 받음각 증가로 나셀 바깥쪽 날개 부분은 조기에 실속에 잠김을 알 수 있었다. 프로펠러는 날개의 inboard에서 하강하는 회전 방향이 프로펠러 후류로 인한 실속 지연 측면에서 유리함을 알 수 있었다.

• Journal of Trauma and Injury
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• 제26권1호
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• pp.14-17
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• 2013

Purpose: The open abdomen is now the standard of care in various clinical situations, especially it is used to treat abdominal compartment syndrome. Many techniques have been reported for closure after an open abdomen, but most take a long time for complete definitive closure and are associated with various problems. We describe a technique using biologic mesh that can achieve early definitive closure after an open abdomen. Methods: A 45-year-old man presented to the emergency room with a painful hip and painful lower extremities after a fall from 80 feet. Radiologic examination revealed multiple fractures of the pelvis and low extremities. Abdominal compartment syndrome caused by a retroperitoneal hematoma developed during the orthopedic surgery. We performed exploration immediately and closed abdomen temporarily. A peritoneal graft of porcine dermal collagen with anterior myofascial approximation of the rectus abdominis muscles and sliding skin flap was performed three days after the previous surgery. Results: There were no complications related to the wound. The patient was transferred to the Department of Orthopedic Surgery seven days after the initial surgery. Conclusion: Early definitive closure using porcine dermal collagen is a feasible method that can reduce the length of hospitalization and the number of operations for an open abdomen.

• International Journal of Fluid Machinery and Systems
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• 제2권2호
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• pp.110-120
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• 2009

Generally the fluid flows within the centrifugal impeller passage as a decelerating flow with an adverse pressure gradient along the stream wise path. This flow tends to be in a state of instability with flow separation zones on the suction surface and on the front shroud. Hence several experimental attempts were earlier made to assess the efficacy of using boundary layer fences to trip the flow in the regions of separation and to make the flow align itself into stream wise direction so that the losses could be minimized and overall efficiency of the diffusion process in the fan could be increased. With the development of CFD, an extensive numerical whole field analysis of the effect of boundary layer fences in discrete regions of suspected separation points is possible. But it is found from the literature that there have been no significant attempts to use this tool to explore numerically the utility of the fences on the flow field. This paper attempts to explore the effect of boundary layer fences corresponding to various geometrical configurations on the impeller as well as on the diffuser. It is shown from the analysis that the fences located on the impellers near the trailing edge on pressure side and suction side improves the static pressure recovery across the fan. Fences provided at the radial mid-span on the pressure side of the diffuser vane and near the leading edge and trailing edge of the suction side of diffuser vanes also improve the static pressure recovery across the fan.

• International Journal of Naval Architecture and Ocean Engineering
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• 제5권3호
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• pp.333-347
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• 2013

The present study numerically models the interaction between a regular wave and the roll motion of a rectangular floating structure. In order to simulate two-dimensional incompressible viscous two-phase flow in a numerical wave tank with the rectangular floating structure, the present study used the volume of fluid method based on the finite volume method. The sliding mesh technique is adopted to handle the motion of the rectangular floating structure induced by fluid-structure interaction. The effect of the wave period on the flow, roll motion and forces acting on the structure is examined by considering three different wave periods. The time variations of the wave height and the roll motion of the rectangular structure are in good agreement with experimental results for all wave periods. The present response amplitude operator is in good agreement with experimental results with the linear potential theory. The present numerical results effectively represent the entire process of vortex generation and evolution described by the experimental results. The longer wave period showed a different mechanism of the vortex evolution near each bottom corner of the structure compared to cases of shorter wave periods. In addition, the x-directional and z-directional forces acting on the structure are analyzed.