• 한국전산유체공학회지
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• 제20권2호
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• pp.16-22
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• 2015

The pressure is generally lower than that of the freestream at the base of a missile body due to the energy loss by the flow separation around the edge of the base. The base pressure changes in the presence of the thrust jet due to the interaction between the base flow of the missile and the jet flow. In this study, behavior of the missile base pressure by the change of the jet exit pressure and the freestream condition is investigated using the CFD(Computational Fluid Dynamics) method. Effects of the grid type and the freestream condition are tested. The results are compared with the semi-empirical predictions and the flight test data. The CFD results agree well with the flight test data. The semi-empirical predictions overestimate the base pressure when jet thrust is strong for low freestream speed.

• 산업융합연구
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• 제21권7호
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• pp.83-92
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• 2023

유전체 전위장벽방전방식에 의한 플라즈마 젯의 블렛 형상은 인가되는 유량과 전기장의 크기에 따라 달라지고 이러한 변화는 DBD 플라즈마 젯의 밀도차이에 의한 스펙트럼 분포의 차이로 나타난다. 발생된 플라즈마 젯의 스펙트럼의 분석을 통한 활성종의 발생과 강도의 차이는 장치를 활용하는데 있어서 중요한 요소이다. 본 논문에서는 Ar가스를 이용한 대기압 볼륨 DBD방식의 플라즈마 젯 발생장치를 제안된 설계방법에 따라 구성하였다. 플라즈마 젯의 발생을 위한 유량의 의존도를 규명하기 위한 Ar가스의 유동해석을 시뮬레이션을 통해 확인하였고 프로토타입 시스템에서는 MFC를 통한 유량제어를 통해 최적의 플라즈마 젯 불렛형상을 발생시키고 발생된 플라즈마 젯의 특성을 분석하기 위해 스펙트로미터를 이용한 플라즈마 젯의 특성을 분석하였다. 제안된 시스템의 설계방법을 통한 장치에서 최적의 플라즈마 젯 형상 확립방법과 EOS 상에서 활성종에 대한 결과를 확인하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.221-224
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• 2002

A technique of mixing enhancement in an underexpanded sonic round jet is studied with fully expanded jet Mach number 1.5. Tonal sound, jet screech can be produced at some underexpansion pressure ratio in a sonic jet. Since the jet screech excites the initial Jet shear layer to change the flow, a reflector which focuses the jet screech near the nozzle lip is designed. The reflector has an elliptic shape of which two foci are located near the nozzle lip and the jet screech source region. Jet screech tone near the nozzle lip increases with the elliptic reflector and spreading of the jet largely increases. It is concluded that mixing enhancement of the jet with the elliptic reflector is attributed to large scale structures which are initially excited by the increased jet screech.

• 한국압력기기공학회 논문집
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• 제13권2호
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• pp.51-59
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• 2017

Steam jets ejected from a rupture zone of high energy pipes may cause damage to adjacent structures. This event could lead to more serious accidents in nuclear power plants. Therefore, to prevent serious accidents, high energy pipes of nuclear power plants are designed according to the ANSI / ANS 58.2 technical standard. However, the US Nuclear Regulatory Commission (USNRC) has recently pointed out non-conservatism in existing high energy pipe fracture evaluation methods, and required the assessment of the unsteady load of the jet caused by a potential feedback mechanism as well as the impact range of steam jet, the jet impact loads and the blast wave effects at the initial breakage stage. The potential feedback mechanism refers to a phenomenon in which a vortex formed by impingement jets amplifies vortex itself and induces jet vibration in a shear layer. In this study, CFD methodology using the LES turbulence model is established and numerical analysis is carried out to evaluate the dynamic behavior of impingement jets and the potential feedback mechanism during jet impingement. Obtained results have been compared with an empirical correlation and experiment.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.622-627
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• 2008

Experiment of active noise control on supersonic jet noise was conducted by use of microjet injection. The microjets were injected to the shear layer of the main jet through 22 small holes at the lip of a rectangular nozzle. Based on the measurement of farfield sound pressure, it was found that the jet noise was effectively reduced by several dB(in some cases up to 10 dB). The power levels of all measurement points were also reduced by use of microjet injection. The microjet affected not only the broadband noise but also the screech tone noise. The sound pressure level, the frequency of the screech tone, and the structure of the jet could be changed by the microjet. Flow visualization with schlieren technique was also made to observe the effect of microjet on the flow field.

• 한국추진공학회지
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• 제24권5호
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• pp.1-12
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• 2020

본 논문에서는 재생냉각 연소기에서 냉각제 및 연료로 사용되는 Jet A-1의 열전달 특성에 대해 실험적으로 연구하였다. 냉각채널 가열을 위한 인가 전류, 모사 시편 지름, 시편 후단 압력, Jet A-1 유속을 변화시키며, 시편에서의 벽면 온도 및 시편 전/후단에서의 Jet A-1 온도를 측정하였다. 시편 지름과 유속이 열전달 특성에 중요한 인자임을 알 수 있었으며, 시편의 후단 압력은 열전달 성능에 영향을 주지 않음을 확인할 수 있었다. 열전달 실험결과는 기존 Nu수 경험식들과 비교하였으며, 최종적으로 새로운 Nu수 경험식을 도출하였다.

• 한국추진공학회지
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• 제13권2호
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• pp.1-8
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• 2009

횡단류로 펄스 분사되는 액체제트의 분무 특성을 연구하기 위하여 35.7 ~ 166.2Hz 범위의 분사 주파수와 횡단류 속도 42 ~ 136 m/s의 조건에서 실험을 수행하였다. 횡단 유동장에서 액체제트의 주된 분열 인자는 압력 펄스 주파수의 영향보다는 횡단류의 항력에 의존하며, 주기적인 압력 진동에 의해 횡단류로 분사된 액체제트는 상하 진동하는 특성을 나타냈다. 또한 액적의 집합체(liquid jet puff)가 횡단류 방향의 액체 제트 표면에 나타났으며, 이러한 두 가지 특성을 통해 유동장의 혼합을 예상할 수 있었다. 압력 펄스 주파수에 의한 SMD 특성은 연속 분사의 층상 구조와 다른 비층상 구조로 나타났으며, 체적 유속은 압력 펄스 주파수가 증가함에 따라 감소하는 경향을 나타내었다.

• 한국전산유체공학회지
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• 제2권2호
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• pp.44-50
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• 1997

Accurate simulation of jet plume exhausting into the open space as well as onto the opposing wall is of interest both numerically and physically; the latter, from a system designer's point of view. In the current work, Navier-Stokes computation is undertaken to capture the flow pattern of a supersonic jet impinging onto a rectangular duct which deflects the vertical jet horizontally. Of particular interest are the flow structure in the jet exhaust area, pressure pattern and the magnitude of pressure force at the bottom wall. Usefulness of present characteristic boundary condition applied at the exiting plane of the duct is demonstrated by capturing such complex flow structures for different lengths of the deflection duct.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1997년도 추계 학술대회논문집
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• pp.136-142
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• 1997

The present study is aimed to investigate flow characteristics of confined jet flow within circular pipe. Numerical method based upon revised SOLA scheme which secures conservation form of convective terms on irregular grids by interpolating the variables appearing in staggered meshes is adopted on cylindrical coordinate formation. Computation was carried out for two kinds of Reynolds number, $10^5\;and\;1.5{\times}10^5$ defined by diameter of outer pipe and time-mean driving jet velocity. Results show that periodic vortex shedding from the jet mixing layer is profound and related unsteady flow characteristics prevail over the entire region. Spatial distribution of pressure and kinetic energy, fluctuation of static wall pressure, together with radial velocity components are examined in terms of instantaneous and time-mean point of views.

• 대한기계학회논문집
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• 제18권11호
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• pp.3021-3031
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• 1994

Experiments have been performed to find out the effect of the mixing port length of Y-jet atomizers on the spray performance, using air and water as the test fluids. Water and air flow rates and drop sizes were measured at each injection pressure condition for different mixing port length. The air flow rate was almost unaffected by the change of the mixing port length. However, the water flow rate was relatively susceptible to the change of the mixing port length. The mixing point pressure was very much influenced by the mixing port length. Variations of spatial distribution of Sauter Mean Diameter (SMD, $D_{32}$) and the cross-section-averaged SMD ($D_{32,m}$) with different mixing port length and air/water mass flow rate ratio were examined. Generally, when the mixing port length was reduced, the mean drop size decreased and became spatially even.