• 제목/요약/키워드: Dynamic Pressure

검색결과 2,450건 처리시간 0.038초

입자크기 분포를 고려한 부력침강 저수지 밀도류의 탁도 모델링 (Turbidity Modeling for a Negative Buoyant Density Flow in a Reservoir with Consideration of Multiple Particle Sizes)

  • 정세웅;이흥수;정용락
    • 한국물환경학회지
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    • 제24권3호
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    • pp.365-377
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    • 2008
  • Large artificial dam reservoirs and associated downstream ecosystems are under increased pressure from long-term negative impacts of turbid flood runoff. Despite various emerging issues of reservoir turbidity flow, turbidity modeling studies have been rare due to lack of experimental data that can support scientific interpretation. Modeling suspended sediment (SS) dynamics, and therefore turbidity ($C_T$), requires provision of constitutive relationships ($SS-C_T$) and accounting for deposition of different SS size fractions/types distribution in order to display this complicated dynamic behavior. This study explored the performance of a coupled two-dimensional (2D) hydrodynamic and particle dynamics model that simulates the fate and transport of a turbid density flow in a negatively buoyant density flow regime. Multiple groups of suspended sediment (SS), classified by the particle size and their site-specific $SS-C_T$ relationships, were used for the conversion between field measurements ($C_T$) and model state variables (SS). The 2D model showed, in overall, good performance in reproducing the reservoir thermal structure, flood propagation dynamics and the magnitude and distribution of turbidity in the stratified reservoir. Some significant errors were noticed in the transitional zone due to the inherent lateral averaging assumption of the 2D hydrodynamic model, and in the lacustrine zone possibly due to long-term decay of particulate organic matters induced during flood runoffs.

Intelligent Phase Plane Switching Control of Pneumatic Artificial Muscle Manipulators with Magneto-Rheological Brake

  • Thanh, Tu Diep Cong;Ahn, Kyoung-Kwan
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2005년도 ICCAS
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    • pp.1983-1989
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    • 2005
  • Industrial robots are powerful, extremely accurate multi-jointed systems, but they are heavy and highly rigid because of their mechanical structure and motorization. Therefore, sharing the robot working space with its environment is problematic. A novel pneumatic artificial muscle actuator (PAM actuator) has been regarded during the recent decades as an interesting alternative to hydraulic and electric actuators. Its main advantages are high strength and high power/weight ratio, low cost, compactness, ease of maintenance, cleanliness, readily available and cheap power source, inherent safety and mobility assistance to humans performing tasks. The PAM is undoubtedly the most promising artificial muscle for the actuation of new types of industrial robots such as Rubber Actuator and PAM manipulators. However, some limitations still exist, such as the air compressibility and the lack of damping ability of the actuator bring the dynamic delay of the pressure response and cause the oscillatory motion. In addition, the nonlinearities in the PAM manipulator still limit the controllability. Therefore, it is not easy to realize motion with high accuracy and high speed and with respect to various external inertia loads in order to realize a human-friendly therapy robot To overcome these problems a novel controller, which harmonizes a phase plane switching control method with conventional PID controller and the adaptabilities of neural network, is newly proposed. In order to realize satisfactory control performance a variable damper - Magneto-Rheological Brake (MRB) is equipped to the joint of the manipulator. Superb mixture of conventional PID controller and a phase plane switching control using neural network brings us a novel controller. This proposed controller is appropriate for a kind of plants with nonlinearity uncertainties and disturbances. The experiments were carried out in practical PAM manipulator and the effectiveness of the proposed control algorithm was demonstrated through experiments, which had proved that the stability of the manipulator can be improved greatly in a high gain control by using MRB with phase plane switching control using neural network and without regard for the changes of external inertia loads.

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PI 제어기를 이용한 초음속 엔진 버즈마진 및 추력제어에 관한 연구 (A Study on Buzz Margin and Thrust Control of Supersonic Engine using PI Controller)

  • 공창덕;기자영;고성희
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 제33회 추계학술대회논문집
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    • pp.573-577
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    • 2009
  • 초음속제트 엔진의 동적거동 모사를 수행하고 흡입구에서의 버즈 마진 확보와 추력 제어를 위한 PI 제어 알고리즘을 연구하였다. 먼저 연료유량 제어를 통해 요구추력을 추종하고 노즐 목 면적 제어를 통해 흡입구에서의 버즈마진이 항상 양의 수를 갖도록 흡입구 출구 압력을 조절하였다. 비행 마하 수, 고도, 받음각 변화에 따라 추력제어와 버즈 마진 제어를 위한 비례 게인과 적분 게인을 각각 구하고 시뮬레이션 하였다. 그 결과 비행 마하 수 2.1에서 3.0, 받음각 $0^{\circ}$에서 $10^{\circ}$ 사이의 운용영역에서 제어목표를 만족함을 확인하였다.

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PID 제어기를 이용한 초음속 엔진 흡입구의 버즈마진 제어에 관한 연구 (A Study on Buzz Margin Control in Supersonic Engine Intake using PID Controller)

  • 공창덕;기자영;고성희;강명철
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 춘계학술대회 논문집
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    • pp.88-92
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    • 2009
  • 초음속 추진기관은 기계적인 압축기를 통해 흡입공기를 압축하는 방식이 아니라 램 압축 현상을 이용하여 흡입공기를 압축하기 때문에 흡입구에서의 전압력 회복율이 초음속 추진기관 전체의 작동특성에 결정적인 영향을 주게 된다. 제어기 설계에 앞서 엔진의 동특성 해석을 수행한 결과 비행체의 받음각이 커질수록 버즈마진 값이 작아져 일부영역에서는 충격파가 흡입구 외부에서 발생하게 됨을 확인할 수 있었다. 따라서 흡입구 내의 충격파 특성이 성능요구조건을 만족할 수 있도록 버즈마진을 제어하기 위한 PID 제어알고리즘을 설계하였다. 제어변수는 연료유량과 노즐 목면적이며 버즈마진 값이 양의 값을 갖도록 PID 제어기를 설계하였다.

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케로신-공기 혼합물의 데토네이션 하중에 의한 열탄소성 관의 동적 거동 해석 (Numerical Investigation of Dynamic Responses of a Thermal Elasto-plastic Tube under Kerosene-air Mixture Detonation)

  • 곽민철;이영헌;여재익
    • 한국추진공학회지
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    • 제20권5호
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    • pp.60-69
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    • 2016
  • 본 연구에서는 케로신-공기 혼합물 데토네이션 계산과 다물질 해석을 기반으로 데토네이션 하중에 의한 얇은 금속관의 열탄소성 거동에 대한 수치계산을 수행하였다. 데토네이션 하중은 케로신-공기 혼합물의 데토네이션을 활용하여 모델링하였으며, 검증을 위해 해석 결과를 C-J 조건과 실험적 셀 직경을 통해 비교 검증하였다. 또한 금속의 탄성/소성 거동을 확인하기 위하여, 소성 거동은 구리의 Taylor impact 문제로, 탄성 거동은 베를리움 평판 떨림 문제를 활용하였다. 온도에 의한 관의 탄소성 거동 변화를 확인하기 위하여 동일한 데토네이션 하중 하에서 초기 온도가 다른 관의 거동을 확인하고 이론식과의 비교를 통해 열연화 효과가 고려되어야 함을 확인하였다.

외식사업발전을 위한 조리분야 아웃소싱 전략에 관한 연구 (평가측정치 개발절차를 중심으로) (A Comparative Study of Outsourcing Culinary Part of Foodservice Industry Development.)

  • 김기영
    • 한국조리학회지
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    • 제7권3호
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    • pp.13-34
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    • 2001
  • The case which it contracts with the dynamic result measurement system when actual outsourcing evaluation measurement is composed and then one result standard between the service supplier and the user is set, which owns jointly the expense which is reduced from that or the benefit which is created from that is increasing In the conclusion, for outsourcing management strategy of domestic foodservice industry in order to succeed, first it is accurate and examined that for what and how outsourcing should be introduced and as a result, what kind of result can be raised from that result\ulcorner Food service industry should be outsourced if you want to make more many investment in better humane resources, food & beverage-goods-security and education to provide eating-out service out of various business in food industry. When considering the actuality of the domestic foodservice industry that time it is appropriate, it sees. The foreign-brand goods which is introduced in the country are being executing in the 1ink of part management strategy. One of the most influential factor of domestic foodservice industry's management pressure is overspent management expenses, Does the namely expenses preparation effect reach which degree\ulcorner what kind of method can most decrease these expenses\ulcorner Doing grows the success and failure of the Korean foodservice industry controls result with the fact that it will operate with a big variable sees. The background which the domestic foodservice industry should introduce inevitably the outsiurcing system is to develop continuously nation foodservice industry in the way of cost curtailment of food-material, a labor cost curtailment with efficient application and synergic effect like specialty manpower utilization. The kindred competitive enterprises gradually concentrate management resource to the point ability from the present point of view which is increasing and a strategy position they secure, to prepare a competitive power, what sees it is important national industry must prepare a new paradigm. It is important to measure the result based on sales accomplishment in operation system dimension, and it is more important to appropriately apply regard of the evaluation measurement

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Rotordynamic Characteristics of Floating Ring Seals in Rocket Turbopumps

  • Tokunaga, Yuichiro;Inoue, Hideyuki;Hiromatsu, Jun;Iguchi, Tetsuya;Kuroki, Yasuhiro;Uchiumi, Masaharu
    • International Journal of Fluid Machinery and Systems
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    • 제9권3호
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    • pp.194-204
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    • 2016
  • Floating ring seals offer an opportunity to reduce leakage flows significantly in rotating machinery. Accordingly, they have been applied successfully to rotating machinery within the last several decades. For rocket turbopump applications, fundamental behavior and design philosophy have been revealed. However, further work is needed to explore the rotordynamic characteristics associated with rotor vibrations. In this study, rotordynamic forces for floating ring seals under rotor's whirling motions are calculated to elucidate rotordynamic characteristics. Comparisons between numerical simulation results and experiments demonstrated in our previous report are carried out. The three-dimensional Reynolds equation is solved by the finite-difference method to calculate hydrodynamic pressure distributions and the leakage flow rate. The entrance loss at the upstream inlet of the seal ring is calculated to estimate the Lomakin effect. The friction force at the secondary seal surface is also considered. Numerical simulation results showed that the rotordynamic forces of this type of floating ring seal are determined mainly by the friction force at the secondary seal surface. The seal ring is positioned almost concentrically relative to the rotor by the Lomakin effect. Numerical simulations agree quite well with the experimental results.

다중효용 담수설비용 열압축기의 디퓨져 입구부 형상에 관한 연구 (A Study on the Diffuser Inlet Shape of Thermocompressor for MED Desalination Plant)

  • 김창복;송영호;김경근;박기태;정한식;최두열
    • Journal of Advanced Marine Engineering and Technology
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    • 제32권6호
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    • pp.869-876
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    • 2008
  • A thermocompressor is the equipment which compresses a vapor to a desired discharge pressure. Since it was first used as the evacuation pump for a surface condenser, it has been widely adopted for energy saving systems due to its high working confidence. In the present study, the geometrical analysis of the shape between the jet nozzle and the diffuser inlet, the drag force was calculated by means of the integrated equation of motion and the computational fluid dynamic (CFD) package called FLUENT. The computer simulations were performed to investigate the effects by the various suction flow rates, the distance from jet nozzle outlet to the diffuser inlet and the dimensions of the diffuser inlet section through the iterative calculation. In addition, the results from the CFD analysis on the thermocompressor and the experiments were compared for the verification of the CFD results. In the case of a jet nozzle, the results from the CFD analysis showed a good agreement with the experimental results. Furthermore, in this study, a special attention was paid on the performance of the thermocompressor by varying the diffuser convergence angle of $0.0^{\circ}$, $0.5^{\circ}$, $1.0^{\circ}$, $2.0^{\circ}$, $3.5^{\circ}$ and $4.5^{\circ}$. With the increase of the diffuser convergence angle. the suction capacity was improved up to the degree of $1.0^{\circ}$ while it was decreased over the degree of $1.0^{\circ}$.

고체로켓모터의 비선형 연소 불안정성 예측 기법 (The Nonlinear Combustion Instability Prediction of Solid Rocket Motors)

  • 홍지석;문희장;성홍계;엄원석;서성현;이도형
    • 한국추진공학회지
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    • 제20권1호
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    • pp.20-27
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    • 2016
  • 연소 불안정 현상은 연료의 응답 함수, 연소율, 국부 연료 표면의 유동 속도에 영향을 미치기 때문에 고체로켓 모터 설계 시 성능이나 구조적 안정성을 다루는 측면에서 매우 중요한 부분이다. 연소 불안정 현상은 음향 모드가 연소/유동과정에서 발생하는 진동수와 결합(coupled)되었을 때 발생한다. 본 연구에서는 비선형 파동방정식으로부터 음향 비선형 불안정 모델을 유도하여 실린더형 고체로켓 모터의 연소 불안정 현상을 분석하였다. 또한 고체로켓 모터 연소실 압력, 연소 속도가 연소 불안정에 미치는 영향을 조사하였다.

Effect of impingement edge geometry on the acoustic resonance excitation and Strouhal numbers in a ducted shallow cavity

  • Omer, Ahmed;Mohany, Atef;Hassan, Marwan
    • Wind and Structures
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    • 제23권2호
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    • pp.91-107
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    • 2016
  • Flow-excited acoustic resonance in ducted cavities can produce high levels of acoustic pressure that may lead to severe damage. This occurs when the flow instability over the cavity mouth, which is created by the free shear layer separation at the upstream edge, is coupled with one of the acoustic modes in the accommodating enclosure. Acoustic resonance can cause high amplitude fluctuating acoustic loads in and near the cavity. Such acoustic loads could cause damage in sensitive applications such as aircraft weapon bays. Therefore, the suppression and mitigation of these resonances are very important. Much of the work done in the past focused on the fluid-dynamic oscillation mechanism or suppressing the resonance by altering the edge condition at the shear layer separation. However, the effect of the downstream edge has received much less attention. This paper considers the effect of the impingement edge geometry on the acoustic resonance excitation and Strouhal number values of the flow instabilities in a ducted shallow cavity with an aspect ratio of 1.0. Several edges, including chamfered edges with different angles and round edges with different radii, were investigated. In addition, some downstream edges that have never been studied before, such as saw-tooth edges, spanwise cylinders, higher and lower steps, and straight and delta spoilers, are investigated. The experiments are conducted in an open-loop wind tunnel that can generate flows with a Mach number up to 0.45. The study shows that when some edge geometries, such as lower steps, chamfered, round, and saw-tooth edges, are installed downstream, they demonstrate a promising reduction in the acoustic resonance. On the other hand, higher steps and straight spoilers resulted in intensifying the acoustic resonance. In addition, the effect of edge geometry on the Strouhal number is presented.