• 한국추진공학회지
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• 제21권1호
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• pp.51-62
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• 2017

RBCC 엔진의 공기흡입 모드 추진성능을 결정하는 주요 요소인 유로 형상 설계를 위하여 최적설계 기법을 적용하였다. Kriging 모델 기반의 유전자 알고리즘을 이용하여 RBCC 엔진의 비추력을 최대로 하는 최적화를 수행하였으며, 분산분석법과 자가조직도를 통해 설계결과를 분석하였다. 램제트 및 스크램제트의 설계 조건을 각각 고도 20 km, 마하수 4 및 30 km, 마하수 7 설정하여 최적화를 수행한 결과, 기본 형상에 비해 각 모드에서 약 7% 및 10%의 비추력 상승을 얻을 수 있었다.

• Animal Bioscience
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• 제34권5호
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• pp.922-930
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• 2021

Objective: Tibetan pigs, predominantly originating from the Tibetan Plateau, have been subjected to long-term natural selection in an extreme environment. To characterize the metabolic adaptations to hypoxic conditions, transcriptomic and proteomic expression patterns in the livers of Tibetan and Yorkshire pigs were compared. Methods: RNA and protein were extracted from liver tissue of Tibetan and Yorkshire pigs (n = 3, each). Differentially expressed genes and proteins were subjected to gene ontology and Kyoto encyclopedia of genes and genomes functional enrichment analyses. Results: In the RNA-Seq and isobaric tags for relative and absolute quantitation analyses, a total of 18,791 genes and 3,390 proteins were detected and compared. Of these, 273 and 257 differentially expressed genes and proteins were identified. Evidence from functional enrichment analysis showed that many genes were involved in metabolic processes. The combined transcriptomic and proteomic analyses revealed that small molecular biosynthesis, metabolic processes, and organic hydroxyl compound metabolic processes were the major processes operating differently in the two breeds. The important genes include retinol dehydrogenase 16, adenine phosphoribosyltransferase, prenylcysteine oxidase 1, sorbin and SH3 domain containing 2, ENSSSCG00000036224, perilipin 2, ladinin 1, kynurenine aminotransferase 1, and dimethylarginine dimethylaminohydrolase 1. Conclusion: The findings of this study provide novel insight into the high-altitude metabolic adaptation of Tibetan pigs.

• 한국임상수의학회지
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• 제36권1호
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• pp.23-29
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• 2019

While research findings suggest that the highly pathogenic avian influenza (HPAI) is the leading cause of economic loss in Korean poultry industry with an estimated cumulative impact of $909 million since 2003, identifying the environmental and anthropogenic risk factors involved remains a challenge. The objective of this study was to identify areas at high risk for potential HPAI outbreaks according to the likelihood of HPAI virus detection in wild birds. This study integrates spatial information regarding HPAI surveillance with relevant demographic and environmental factors collected between 2003 and 2018. The Maximum Entropy (Maxent) species distribution modeling with presence-only data was used to model the spatial risk of HPAI virus. We used historical data on HPAI occurrence in wild birds during the period 2003-2018, collected by the National Quarantine Inspection Agency of Korea. The database contains a total of 1,065 HPAI cases (farms) tied to 168 unique locations for wild birds. Among the environmental variables, the most effective predictors of the potential distribution of HPAI in wild birds were (in order of importance) altitude, number of HPAI outbreaks at farm-level, daily amount of manure processed and number of wild birds migrated into Korea. The area under the receiver operating characteristic curve for the 10 Maxent replicate runs of the model with twelve variables was 0.855 with a standard deviation of 0.012 which indicates that the model performance was excellent. Results revealed that geographic area at risk of HPAI is heterogeneously distributed throughout the country with higher likelihood in the west and coastal areas. The results may help biosecurity authority to design risk-based surveillance and implementation of control interventions optimized for the areas at highest risk of HPAI outbreak potentials.

• 한국항공운항학회지
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• 제26권4호
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• pp.36-42
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• 2018

Although continuous passenger injuries and physical damages are repeated due to the unexpected aviation turbulence encountered during operations, there is still exist the limitation for preventing recurrence of similar events because the lack of real-time information and delay in technological developments regarding various operating conditions and variable weather phenomena. The purpose of this study is to compare and analyze the meteorological data of the aviation turbulence occurred and actual flight data extracted from the Quick Access Recorder(QAR) to provide some precursors that the pilot can identify aviation turbulence early by referring thru the flight instrumentation indications. The case applied for this study was recent event, a scheduled flight from Incheon Airport, Korea to Narita Airport, Japan that suddenly encountered turbulence at an altitude of approximately 14,000 feet during approach. According to the Korea Meteorological Administration(KMA)'s Regional Data Assessment and Prediction System(RDAPS) data, it was observed that the strong amount of vorticity in the rear area of jet stream, which existed near Mount Fuji at that time. The QAR data analysis shows significant changes in the aircraft's parameters such as Pitch and Roll angle, Static Air Temperature(SAT), and wind speed and direction in tens of seconds to minutes before encounter the turbulence. If the accumulate reliability of the data in addition and verification of various parameters with continuous analysis of additional cases, it can be the precursors for the pilot's effective and pre-emptive action and conservative prevention measures against aviation turbulence to reduce subsequent passenger injuries in the aviation operations.

• 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.

• 한국항공우주학회지
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• 제47권1호
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• pp.49-58
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• 2019

과학기구는 임무 종료시 전체 플랫폼의 안정적인 회수가 가능한 비행 시스템이다. 과학기구의 회수는 인명 및 재산피해를 고려하여 인구밀집도가 낮은 평야지대에서 주로 진행된다. 하지만 대한민국의 경우 밀집한 산악지형과 반도의 제한으로 인해 해상회수가 고려되어야 한다. 이러한 운용환경에서 기낭은 해상 착수 후 발생할 수 있는 심각한 해양오염 때문에 반드시 회수되어야 한다. 따라서 본 논문에서는 기낭의 위치추적기 및 방수체계가 결합된 분리장치를 개발하였다. 장치는 데이터 송수신, 분리, 방수 체계로 구성되었고 대한민국의 환경을 고려하여 제작하였다. 장치의 성능과 기낭의 낙하 궤적은 목표고도 20km 플랫폼의 분리 실험과 영압력 기구의 해상회수를 진행하여 검증하였다.

• 한국전자통신학회논문지
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• 제17권5호
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• pp.767-774
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• 2022

본 논문에서는 우리나라에서 운용 중인 4개 제조사 윈드프로파일러의 성능 평가 및 품질관리의 방향성을 제시하기 위해 원시 스펙트럼 자료를 분석하였다. 계절별로 평균한 스펙트럼의 프로파일과 파워 스펙트럼 밀도(PSD, Power Spectrum Density)로 산출한 4가지 통계값(최소, 평균, 중앙, 최댓값)의 프로파일을 활용하였다. 스펙트럼 자료의 품질은 LAP-3000이 가장 우수하였고, YKJ3, PCL-1300, CLC-11-H가 뒤를 이었다. 철원과 추풍령에 설치된 PCL-1300은 지형과 비기상 신호로 인한 스펙트럼의 변동성이 커서 지형 클러터 제거와 이동평균, 멀티피크 등의 신호처리 과정이 요구되었다. 군산과 파주에 설치된 CLC-11-H는 직류 치우침과 전파거리 접힘 현상이 발견되어 직류 치우침 제거와 관측 유효 고도 제한이 선행될 필요가 있다.

• 문화기술의 융합
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• 제9권3호
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• pp.287-292
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• 2023

미국 항공우주국(NASA)은 저고도의 공중을 새롭게 구축하고자 도시의 단거리 항공 운송 생태계를 새로운 개념의 도심항공모빌리티(Urban Air Mobility, UAM)을 제시하여 현재 UAM이라는 용어가 전 세계적으로 통용되고 있다. 이러한 패러다임은 우리나라 정부에서도 2025년까지 도심항공교통 서비스 상용화를 목표로 추진하고 있는 실정이며 더 나아가 급변하는 미래 작전환경 및 전장 공간의 확장으로 공중기동·수송능력 확보 필요성이 대두되고 있어 우리나라 군 조직에서도 필요성이 제기되는 부분이다. 즉, 본 연구는 미 공군의 'Agility Prime' 프로그램을 소개하여 군사적 필요성과 군사적 운용방안에 대해 제시하고자 출발한 연구이며 연구의 체계는 도심항공 모빌리티 배경 및 개념, 한국형 도심항공 모빌리티 발전 추세, 미 공군의 'Agility Prime' 프로그램 분석 순으로 구성하였으며 본 연구에 이어서 후속연구로 진행되길 기대한다.

• Journal of Astronomy and Space Sciences
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• 제40권4호
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• pp.199-215
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• 2023

The Korea Pathfinder Lunar Orbiter (KPLO), the first South Korea lunar exploration probe, successfully arrived at the Moon on December, 2022 (UTC), following a 4.5-month ballistic lunar transfer (BLT) trajectory. Since the launch (4 August, 2022), the KPLO magnetometer (KMAG) has carried out various observations during the trans-lunar cruise phase and a 100 km altitude lunar polar orbit. KMAG consists of three fluxgate magnetometers capable of measuring magnetic fields within a ± 1,000 nT range with a resolution of 0.2 nT. The sampling rate is 10 Hz. During the originally planned lifetime of one year, KMAG has been operating successfully while performing observations of lunar crustal magnetic fields, magnetic fields induced in the lunar interior, and various solar wind events. The calibration and offset processes were performed during the TLC phase. In addition, reliabilities of the KMAG lunar magnetic field observations have been verified by comparing them with the surface vector mapping (SVM) data. If the KPLO's mission orbit during the extended mission phase is close enough to the lunar surface, KMAG will contribute to updating the lunar surface magnetic field map and will provide insights into the lunar interior structure and lunar space environment.

• 한국군사과학기술학회지
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• 제27권1호
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• pp.1-7
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• 2024

Weather is one of the main causes of aircraft accidents, and among the phenomena caused by weather, icing is a phenomenon in which an ice layer is formed when an object exposed to an atmosphere below a freezing temperature collides with supercooled water droplets. If this phenomenon occurs in the rotor blades, it causes defects such as severe vibration in the airframe and eventually leads to loss of control and an accident. Therefore, it is necessary to foresee the icing situation so that it can ascend and descend at an altitude without a freezing point. In this study, vibration data in normal and faulty conditions was acquired, data features were extracted, and vibration was predicted through deep learning-based algorithms such as CNN, LSTM, CNN-LSTM, Transformer, and TCN, and performance was compared to evaluate blade icing. A method for minimizing operating loss is suggested.