• 제목/요약/키워드: Variable Area Nozzle

검색결과 20건 처리시간 0.029초

소염상태 근방에서의 대향류 수소확산화염의 구조 (Near-Extinction Structure of Counterflow Nonpremixed Hydrogen-Air Flames)

  • 김후중;김용모
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 1997년도 제15회 KOSCO SYMPOSIUM 논문집
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    • pp.77-87
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    • 1997
  • The axisymmetric Navier-Stokes model together with detailed chemical kinetics and variable transport properties has been applied to analyze the effects of the multidimensional flow on the flame characteristics in the nitrogen-diluted hydrogen counterflow nonpremixed flame. Computations are performed for two nozzle exit area-averaged velocities. Effects of multidimensional flow and strain rate on the near-extinction structure of the highly diluted hydrogen flames are discussed in detail.

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가스터빈엔진을 모의하기 위한 시뮬레이션덕트 설계 연구 (Design Study of a Simulation Duct for Gas Turbine Engine Operations)

  • 임주현;김선제;김명호;김유일;김용련
    • 한국추진공학회지
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    • 제23권1호
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    • pp.124-131
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    • 2019
  • 가스터빈엔진 고도시험설비 운용특성탐색 및 설비튜닝 연구와 유량/추력 측정방안 검증을 위한 엔진 시뮬레이션덕트 설계 연구를 수행하였다. 설비 운용특성 검증은 배압/추력 제어가 필요하므로 Spikecone type의 가변노즐을 적용하였으며, 유량검증용 ISO 쵸킹노즐의 추가장착이 가능토록 설계하였다. 시뮬레이션덕트 주유로 면적은 1D Sizing으로 결정하고, 노즐면적변화에 따른 시뮬레이션덕트 내부 유동특성은 1D/CFD 해석으로 조사하였으며, 해석결과로부터 설비운용특성 탐색 및 유량/추력 검증시험을 위한 공기공급부 시험조건을 도출하였다. Spike 노즐 구동부는 시험 전운용 구간에서 공력하중조건을 견디도록 모터, 리니어 볼스크류 등의 부품모델을 선정하였으며, 시험 시 10 mm/s의 이송속도가 가능하도록 설계하였다.

선형 근사화에 의한 가변추진시스템 내탄도 성능 변화 예측 (Ballistic Performance Variation Prediction of Continuously Variable Thrust Solid Rocket Motor by the Linear Approximation)

  • 김중근;박종호
    • 한국항공우주학회지
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    • 제36권1호
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    • pp.79-85
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    • 2008
  • 일반적으로 고체 추진기관은 안전성, 설계/제작의 용이성 그리고 구조가 간단하다는 장점이 있으나 추진제의 그레인 형상과 노즐목 크기가 결정되면 추력 크기를 임의로 조절하는 것이 불가능하기 때문에 최근 들어 고체 추진기관의 추력을 조절할 수 있는 방법들이 활발하게 연구되고 있다. 본 논문에서는 연소관 압력과 노즐목 크기 변화에 따른 고체 추진기관의 추력 및 주요 내탄도 성능 변화를 선형 근사화로 예측하였으며 내탄도 분석 전용 프로그램(SPP)의 분석 결과와 상호 잘 일치함을 확인하였다.

벽면 충돌 난류 확산화염의 특성 (The Characteristics of Turbulent Diffusion Flame Impinging on the Wall)

  • 박용열;김호영
    • 대한기계학회논문집B
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    • 제23권2호
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    • pp.175-184
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    • 1999
  • A theoretical study on the turbulent round jet diffusion flame impinging on the wall was carried out to predict the characteristics and structure of Impinging jet flame and heat transfer to the wall. Finite chemistry via Arrhenius equation and eddy dissipation model was adopted as a combustion model, and the Favre averaging and $k-{\varepsilon}$ model were Introduced In the theoretical modeling. The SIMPLE algorithm was applied to the calculation. All the transport properties were considered as the variable depending on the temperature and composition. For the parametric study, the distance from nozzle to impinging wall and Reynolds number at nozzle exit were chosen 88 the major parameters. As the results of the present study, the characteristics of flow fields, the distributions of main variables and each chemical species and the flame shapes were obtained. The heat transfer rate from the flame to the wall and the effective heating area were calculated to investigate the Influences of the major parameters on the heat transfer characteristics.

각종 Nozzle을 통하여 저장조내로 유입되는 BUOYANT JETS의 유동해석 (Flow analysis of Buoyant Jets into Storage Tank through Variable Nozzles)

  • 박이동;조운
    • 태양에너지
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    • 제9권2호
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    • pp.42-50
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    • 1989
  • The Buoyant Jets were analysed experimentally changing flow rate (0.0291/s, 0.0371/s, 0.0451/s), ratio of nozzle tip area to throat area (aspect ratio ${\beta}$=0.4, 1.0, 1.9), and also the temperature difference (${\Delta}T=Ti-T{\infty}$) between the temperature of the inflow water into the storage tank ($1m{\times}1m{\times}3m$) and the mean temperature of the water in the storage tank were changed as $25^{\circ}C,\;35^{\circ}C$ and $45^{\circ}C$. The more aspect ratio decreased, the more the trajectories of Buoyant Jets center-line were decreased and not the more the trajectories of Buoyant Jets centerline were influenced by the increment of the difference of the temperature. The more aspect ratio decreased, the more the half widths and dilution ratio of Buoyant Jets were increased and not the more the half widths and dilution ratio of Buoyant Jets were influenced by the increment of the difference of the temperature. Fr number is the factor that can predict the flow pattern over the whole flow field. And yet for the consideration the near field of Buoyant Jets flow pattern is dominated by magnitude of momentum and buoyancy force.

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상온기체 모사장치를 이용한 가변추력 고체추진기관의 압력제어 연구 (A Study on Pressure Control for Variable Thrust Solid Propulsion System Using Cold Gas Test Equipment)

  • 이호성;이도윤;박종승;김중근
    • 한국항공우주학회지
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    • 제37권1호
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    • pp.76-81
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    • 2009
  • 본 논문에서는 가변 추력 고체추진기관을 모사할 수 있는 상온기체 시험장치를 이용하여 고체추진기관의 연소실 압력을 능동적으로 제어할 수 있는 비선형 압력 제어알고리듬을 제안하였다. 제안된 제어기법은 고체추진기관의 비선형성과 시변성을 고려하여 설계되었으며, 압력 및 온도조건 등에 따른 물리적 변수들의 변화를 적응제어 알고리듬을 통하여 보상하였다. 비선형 압력제어 알고리듬의 효과를 상온기체 모사장치를 이용한 압력제어 실험을 통하여 검증하였으며, 실험결과 일반적인 비례 제어기 및 비례-적분 제어기에 비하여 제안된 제어기법이 더 좋은 압력제어 성능을 보임을 확인하였다.

헬륨 기체분류의 정상적 비정상적 거동에 관한 연구 (A Study on Steady and Unsteady Behavior of Helium Jet in the Stationary Atmosphere)

  • 김봉곤;서용권;하종률;권순석
    • 한국자동차공학회논문집
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    • 제1권3호
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    • pp.34-45
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    • 1993
  • This study aims to analyze the mixing characteristics of hydrogen considered as a new fuel for internal combustion engines. As the physical property of helium gas is similar to that of hydrogen, helium gas was used in this study. To analyze the steady and unsteady behavior of jet, helium gas was injected into the stationary atmosphere at the normal temperature and pressure. Concentration of helium gas in the center of jet flow is in inverse proportion with axial distance from the nozzle tip. This agrees with the free jet theory of Schlichting. The relative equation for dimensionless concentration to radial/axial distance the axial distance of potential core region, the cone angle a of the jet flow and the relative equation for arriving distance of the front of jet flow to the lapse of time are obtained. But free jet theory of Schlichting in the dimensionless concentration is not in agreement with the present experimental results of the distance of the radial direction. It needs more study. When the arrival frequency of jet flow is used as a parameter, the transition area changing from unsteady flow area into steady flow area becomes gradually wider downstream, but its ratio for the whole unsteady flow area gradually decreases.

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핀틀 구동속도에 따른 핀틀 추력기의 비정상상태 특성에 대한 실험적 연구 (Experimental Study on Unsteady-state Characteristics of a Pintle Thruster with Variable Pintle Speeds)

  • 황희성;허환일
    • 한국항공우주학회지
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    • 제44권3호
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    • pp.247-255
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    • 2016
  • 본 논문에서는 핀틀 추력기의 비정상상태 특성을 파악하기 위하여 구동기의 속도를 측정하였으며, 정상상태 실험을 통해 비정상상태 실험 시스템을 구성하였다. 비정상상태 실험은 총 3 가지의 구동 속도(3.01 mm/s, 5.65 mm/s, 10.83 mm/s)를 이용하여 진행하였다. 그 결과 핀틀이 후진하는 경우가 전진하는 경우보다 더 빨리 명령 압력 값에 수렴하였으며, 이는 핀틀이 후진하는 경우가 연소실의 압력이 높은 상태로 형성되어 있기 때문이다. 핀틀이 전 후진하는 경우에 추력 곡선에 특이점들이 나타났으며, 이는 연소실 압력과 노즐 목 면적 변화에 기인하여 나타난 질유량 변화로 인한 것이다. 구동 속도가 빠를수록 이러한 현상이 뚜렷하게 나타났다.

Steady-State/Transient Performance Simulation of the Propulsion System for the Canard Rotor Wing UAV during Flight Mode Transition

  • Kong, Changduk;Kang, Myoungcheol;Ki, Jayoung
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.513-520
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    • 2004
  • A steady-state/transient performance simulation model was newly developed for the propulsion system of the CRW (Canard Rotor Wing) type UAV (Unmanned Aerial Vehicle) during flight mode transition. The CRW type UAV has a new concept RPV (Remotely Piloted Vehicle) which can fly at two flight modes such as the take-off/landing and low speed forward flight mode using the rotary wing driven by engine bypass exhaust gas and the high speed forward flight mode using the stopped wing and main engine thrust. The propulsion system of the CRW type UAV consists of the main engine system and the duct system. The flight vehicle may generally select a proper type and specific engine with acceptable thrust level to meet the flight mission in the propulsion system design phase. In this study, a turbojet engine with one spool was selected by decision of the vehicle system designer, and the duct system is composed of main duct, rotor duct, master valve, rotor tip-jet nozzles, and variable area main nozzle. In order to establish the safe flight mode transition region of the propulsion system, steady-state and transient performance simulation should be needed. Using this simulation model, the optimal fuel flow schedules were obtained to keep the proper surge margin and the turbine inlet temperature limitation through steady-state and transient performance estimation. Furthermore, these analysis results will be used to the control optimization of the propulsion system, later. In the transient performance model, ICV (Inter-Component Volume) model was used. The performance analysis using the developed models was performed at various flight conditions and fuel flow schedules, and these results could set the safe flight mode transition region to satisfy the turbine inlet temperature overshoot limitation as well as the compressor surge margin. Because the engine performance simulation results without the duct system were well agreed with the engine manufacturer's data and the analysis results using a commercial program, it was confirmed that the validity of the proposed performance model was verified. However, the propulsion system performance model including the duct system will be compared with experimental measuring data, later.

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불량환경하(不良環境下)에서의 제초제(除草劑) 약해(藥害)와 경감기술(輕減技術) (Herbicidal Phytotoxicity under Adverse Environments and Countermeasures)

  • 권용웅;황형식;강병화
    • 한국잡초학회지
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    • 제13권4호
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    • pp.210-233
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    • 1993
  • The herbicide has become indispensable as much as nitrogen fertilizer in Korean agriculture from 1970 onwards. It is estimated that in 1991 more than 40 herbicides were registered for rice crop and treated to an area 1.41 times the rice acreage ; more than 30 herbicides were registered for field crops and treated to 89% of the crop area ; the treatment acreage of 3 non-selective foliar-applied herbicides reached 2,555 thousand hectares. During the last 25 years herbicides have benefited the Korean farmers substantially in labor, cost and time of farming. Any herbicide which causes crop injury in ordinary uses is not allowed to register in most country. Herbicides, however, can cause crop injury more or less when they are misused, abused or used under adverse environments. The herbicide use more than 100% of crop acreage means an increased probability of which herbicides are used wrong or under adverse situation. This is true as evidenced by that about 25% of farmers have experienced the herbicide caused crop injury more than once during last 10 years on authors' nationwide surveys in 1992 and 1993 ; one-half of the injury incidences were with crop yield loss greater than 10%. Crop injury caused by herbicide had not occurred to a serious extent in the 1960s when the herbicides fewer than 5 were used by farmers to the field less than 12% of total acreage. Farmers ascribed about 53% of the herbicidal injury incidences at their fields to their misuses such as overdose, careless or improper application, off-time application or wrong choice of the herbicide, etc. While 47% of the incidences were mainly due to adverse natural conditions. Such misuses can be reduced to a minimum through enhanced education/extension services for right uses and, although undesirable, increased farmers' experiences of phytotoxicity. The most difficult primary problem arises from lack of countermeasures for farmers to cope with various adverse environmental conditions. At present almost all the herbicides have"Do not use!" instructions on label to avoid crop injury under adverse environments. These "Do not use!" situations Include sandy, highly percolating, or infertile soils, cool water gushing paddy, poorly draining paddy, terraced paddy, too wet or dry soils, days of abnormally cool or high air temperature, etc. Meanwhile, the cultivated lands are under poor conditions : the average organic matter content ranges 2.5 to 2.8% in paddy soil and 2.0 to 2.6% in upland soil ; the canon exchange capacity ranges 8 to 12 m.e. ; approximately 43% of paddy and 56% of upland are of sandy to sandy gravel soil ; only 42% of paddy and 16% of upland fields are on flat land. The present situation would mean that about 40 to 50% of soil applied herbicides are used on the field where the label instructs "Do not use!". Yet no positive effort has been made for 25 years long by government or companies to develop countermeasures. It is a really sophisticated social problem. In the 1960s and 1970s a subside program to incoporate hillside red clayish soil into sandy paddy as well as campaign for increased application of compost to the field had been operating. Yet majority of the sandy soils remains sandy and the program and campaign had been stopped. With regard to this sandy soil problem the authors have developed a method of "split application of a herbicide onto sandy soil field". A model case study has been carried out with success and is introduced with key procedure in this paper. Climate is variable in its nature. Among the climatic components sudden fall or rise in temperature is hardly avoidable for a crop plant. Our spring air temperature fluctuates so much ; for example, the daily mean air temperature of Inchon city varied from 6.31 to $16.81^{\circ}C$ on April 20, early seeding time of crops, within${\times}$2Sd range of 30 year records. Seeding early in season means an increased liability to phytotoxicity, and this will be more evident in direct water-seeding of rice. About 20% of farmers depend on the cold underground-water pumped for rice irrigation. If the well is deep over 70m, the fresh water may be about $10^{\circ}C$ cold. The water should be warmed to about $20^{\circ}C$ before irrigation. This is not so practiced well by farmers. In addition to the forementioned adverse conditions there exist many other aspects to be amended. Among them the worst for liquid spray type herbicides is almost total lacking in proper knowledge of nozzle types and concern with even spray by the administrative, rural extension officers, company and farmers. Even not available in the market are the nozzles and sprayers appropriate for herbicides spray. Most people perceive all the pesticide sprayers same and concern much with the speed and easiness of spray, not with correct spray. There exist many points to be improved to minimize herbicidal phytotoxicity in Korea and many ways to achieve the goal. First of all it is suggested that 1) the present evaluation of a new herbicide at standard and double doses in registration trials is to be an evaluation for standard, double and triple doses to exploit the response slope in making decision for approval and recommendation of different dose for different situation on label, 2) the government is to recognize the facts and nature of the present problem to correct the present misperceptions and to develop an appropriate national program for improvement of soil conditions, spray equipment, extention manpower and services, 3) the researchers are to enhance researches on the countermeasures and 4) the herbicide makers/dealers are to correct their misperceptions and policy for sales, to develop database on the detailed use conditions of consumer one by one and to serve the consumers with direct counsel based on the database.

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