• Title/Summary/Keyword: 이중목

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A Study on the Supersonic Flow Characteristics Through a Dual Throat Nozzle (이중목 노즐에서 발생하는 초음속유동 특성에 관한 연구)

  • Shin, Choon-Sik;Kim, Heuy-Dong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.5
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    • pp.1-7
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    • 2010
  • Dual throat nozzle(DTN) is recently attracting much attention as a new concept of the thrust vectoring technique. This DTN is designed with two throats, an upstream minimum and a downstream minimum at the nozzle exit, with a cavity in between the upstream throat and exit. In the present study, a computational work has been carried out to analyze a fundamental performance of a dual throat nozzle(DTN) at various nozzle pressure ratios(NPR) and throat area ratios. Two-dimensional, axisymmetric, steady, compressible Navier-Stokes equations were solved using a fully implicit finite volume scheme. NPR was varied in the range of NPR from 2.0 to 10.0, at different throat area ratios. The present computational results were validated with some experimental data available. Based upon the present results, the performance of DTN is discussed in terms of the discharge coefficient and thrust efficiency.

A Fundamental Study of Thrust-Vector Control Using a Dual Throat Nozzle (이중목 노즐을 이용한 추력벡터 제어에 관한 기초적 연구)

  • Shin, Choon-Sik;Kim, Heuy-Dong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.6
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    • pp.25-30
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    • 2010
  • Dual throat nozzle(DTN) is recently attracting much attention as a new concept of the thrust vectoring technique. This DTN is designed with two throats, an upstream minimum and a downstream minimum at the nozzle exit, with a cavity in between the upstream throat and exit. In the present study, a computational work has been carried out to analyze the performance of a dual throat nozzle(DTN) at various mass flow rate of secondary flow and nozzle pressure ratios(NPR). Two-dimensional, steady, compressible Navier-Stokes equations were solved using a fully implicit finite volume scheme. The present computational results were validated with some experimental data available. Based upon the present results, The control effectiveness of thrust-vector is discussed in terms of the thrust coefficient and the discharge coefficient.

A Fundamental Study of Thrust-Vector Control Using a Dual Throat Nozzle (이중목 노즐을 이용한 추력벡터 제어에 관한 기초적 연구)

  • Shin, Choon-Sik;Kim, Heuy-Dong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.05a
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    • pp.339-342
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    • 2010
  • Dual throat nozzle(DTN) is recently attracting much attention as a new concept of the thrust vectoring technique of propulsion jet. This DTN is designed with two throats, an upstream minimum and a downstream minimum at the nozzle exit, with a cavity in between the upstream throat and exit. In the present study, a computational work has been carried out to analyze the performance of a dual throat nozzle(DTN) at various mass flow rate of secondary flow. Two-dimensional, steady, compressible Navier-Stokes equations were solved using a fully implicit finite volume scheme. The present computational results were validated with some experimental data available. Based upon the present results, Thrust-vector control using a DTN is discussed in terms of the thrust coefficient and the coefficient of discharge.

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Study on Fluidic Thrust Vector Control Based on Dual-Throat Concept (이중목 노즐 개념에 기반한 유체 추력벡터제어에 관한 연구)

  • Wu, Kexin;Kim, Heuy Dong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.23 no.1
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    • pp.24-32
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    • 2019
  • Numerical simulations were carried out in a supersonic nozzle to investigate the possibility of using dual-throat nozzle concept in fluidic thrust vector control. Validation of the methodology showed an excellent agreement between the computational fluid dynamics results and the experimental data available, which were based on the well-assessed SST $k-{\omega}$ turbulence mode. The deflection angle, system resultant thrust ratio, and thrust efficiency were investigated in a wide range of nozzle pressure ratios and injection pressure ratios. The performance variations of the dual-throat nozzle thrust vector control system were clearly illustrated with this two-dimensional computational domain. Some constructive conclusions were obtained that may be used as a reference for further studies in the fluidic thrust vector control field.

Cervical Vascular Diseases Rarely Observed by Duplex Sonography: 3 Cases (이중초음파에서 드물게 관찰되는 목 부위의 혈관질환: 3례)

  • Han, Minho;Seo, Kangsik;Choi, Junghye
    • Korean Journal of Clinical Laboratory Science
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    • v.53 no.1
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    • pp.131-136
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    • 2021
  • Duplex sonography is used widely in various medical fields because of its repeatability and low cost. In particular, the carotid duplex sonography is a useful non-invasive test for diagnosing cerebrovascular disease and predicting the prognosis. In clinical practice, it is very important to reduce the test time and improve accuracy. The patient's clinical information must be known in advance to perform carotid duplex sonography quickly and accurately. Despite this, there are often difficulties finding new cervical vascular diseases that are not mentioned in the clinical information. Therefore, knowing a variety of cases can lead to fast and accurate results. In this context, this paper reports three cases of cervical vascular disease discovered unexpectedly during carotid duplex sonography: CASE 1, internal carotid artery occlusion and cerebral arteries branched from the external carotid artery; CASE 2, internal jugular vein thrombosis; CASE 3, microembolism observed in the vertebral artery.

Performance Assessment of the Dual-Throat Nozzle Thrust Vector Control in a 3D Rectangular Nozzle (3D 직사각형 노즐에서 이중 스 로트 노즐 스러스트 벡터 제어의 성능 평가)

  • Wu, Kexin;Kim, Tae Ho;Kim, Heuy Dong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.24 no.4
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    • pp.12-24
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    • 2020
  • The dual-throat nozzle is an extremely effective method in the thrust vectoring control field, utilizing another convergent section to connect with the divergent part of the conventional convergent-divergent nozzle. In the present research, the numerical simulation is conducted to investigate the effects of the injection angle on thrust vectoring performance in a 3D supersonic nozzle. Five injection angles are discussed and core performance variations are analyzed, including the deflection angle, injected mass flow ratio, system resultant thrust ratio, efficiency, Mach number contour and streamline on the symmetry plane, and Mach number contours at different slices. Meaningful conclusions are offered for fighter jet designers.

Echinoderms from Geojedo Island and Adjacent Sea Waters, Korea (거제도 해역의 극피동물)

  • Sook Shin
    • Animal Systematics, Evolution and Diversity
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    • v.14 no.3
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    • pp.193-205
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    • 1998
  • The echinoderms collected from 20 localities of Geojedo Island and its adjacent sea waters during the period from February 1995 to May 1998 turned out to be 47 species in 37 genus, 25 familes, 11 orders, three classes. Of which one echinoid species, Prionocidaris baculosa (Lamarck, 1816) is newly added to the Korean fauna of Geojedo Island with 25 previously known species and total 47 species are described in this report.

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Optimal Drive Algorithm Research for Three-Phase BLDC Motor with Double Rotor (이중 회전자 구조를 갖는 3상 BLDC 전동기 최적운전 알고리즘 연구)

  • Jung, Hyun-woo;Kim, Jang-sik;Kim, Jang-mok
    • Proceedings of the KIPE Conference
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    • 2011.11a
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    • pp.10-11
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    • 2011
  • 단일 회전자 전동기와 달리 동일한 크기에서 높은 출력 밀도와 높은 토크의 장점이 있는 이중 회전자 구조를 갖는 전동기는 공간적 제약을 받는 전기 자동차, 전기 이륜차 등의 분야에 활발히 연구되고 있다. 이중 회전자 구조를 갖는 전동기는 고 토크 운전을 위해 이중 인버터 운전 방식이 요구된다. 이때, 내부와 외부전동기의 역기전력이 다를 때 이를 고려하지 않고 운전한다면 발생하는 동손이 증가하여 운전효율 저하로 이어진다. 본 논문에서는 이중 회전자 구조를 갖는 3상 BLDC 전동기에서 내부와 외부전동기의 역기전력비(${\alpha}$)와 고정자 저항 비(${\beta}$)를 고려한 전류분배방식을 통해 동손을 최소화하는 최적운전 알고리즘을 제안하였다.

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