• 한국항공우주학회지
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• 제38권3호
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• pp.274-279
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• 2010

본 논문에서는 원 형상에 비해 20% 축소 설계된 수평 핀을 부착한 전투기의 외부 연료 탱크의 정적인 세로 안정성을 해석하고 투하궤적을 분석하였다. 얇은 에어포일의 공력 자료를 이용하여 연료 탱크의 정적 피칭 안정성을 해석한 결과는 풍동 실험 결과와 거의 일치하였다. 연료탱크의 6자유도 운동방정식에 대한 수치적인 모사에서 얻은 낙하 궤적을 실제 모델의 투하 실험 궤적과 비교 분석한 결과 투하 시 항공기의 자세가 연료 탱크의 수직 이동 궤적에는 영향을 미치지 않지만 수평 이동 궤적에는 상당한 영향을 미치게 됨을 알 수 있었다. 이와 같은 이론 해석 및 실험 결과의 분석을 통해 재설계 핀을 부착한 외부 연료 탱크를 비행 중 항공기로 부터 분리할 때 비행운용 규범을 기준으로 수행한다면 항공기의 안전성을 보장할 수 있음이 검증되었다.

• 항공우주산업기술동향
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• 제6권1호
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• pp.14-24
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• 2008

세계 항공기 산업은 2001년 이후 전반적인 세계경기 회복기조 속에서 꾸준히 성장하고 있다. 9.11사태 이후 시 장 위축과 회복 그리고 유가급등과 환경에 대한 요구 증가 등 근래에 들어 과거와 다른 항공기 산업의 시장환경이 조성되었으며, 이에 따라 항공기 산업 내부에서도 완만한 변화가 이루어져 왔다. 지역 간 직접노선 수요와 비정기 항공에 대한 수요 증가는 200인승 급 대형항공기의 수요증가, 주력 중형항공기의 대형화 및 비즈니스제트기와 VLJ 수요를 촉발하였으며, 항공사간의 경쟁 심화와 유가상승 등은 더욱 효율적인 기체에 대한 요구를 증대시켰다. 군수분야에서는5세대 전투기의 개발 및 채용 확산과 함께 그 이전단계에서 기존의4세대 전투기의 수요 역시 꾸준히 이어지고 있으며, 비정규전 과정을 거치면서 무인 정찰기에 대한 수요 및 접근성이 높은 이동수단에 대한 수요가 증대하였다.

• 한국항행학회논문지
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• 제24권1호
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• pp.9-15
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• 2020

최근 KF-X (Korean Fighter eXperimental)사업에서 AESA (Active electronically scanned array) 레이다, EO-IR (electro-optical and infrared) 및 IRST (infra-red search and track) 센서 등의 개발이 진행되고 있으며 현재 AESA 레이더는 비행 시험을 위한 사전 연구가 진행되고 있다. 본 논문은 AESA 레이다 개발에 따른 선진국의 FTB(Flying Test Bed) 항공기 운영 사례를 중점 분석하고, 이 사례를 중심으로 국내 레이다 개발 시험을 위한 비행시험 항공기의 선정 시 요구사항과 고려사항을 검토하였다. 그에 따른 우리는 FTB 항공기가 국내 환경에서 운영하기 위한 감항 관련 국내 관련 법규를 검토하고 FTB 항공기의 운영하기 위한 방안을 살펴본다. 따라서 우리는 국내 환경에 적합한 FTB 항공기 선정, 감항 및 운영 방안을 제시하고 한다.

• 산업경영시스템학회지
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• 제44권3호
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• pp.39-49
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• 2021

The Korean Air-Force aircraft maintenance depot paints the exterior of various aircraft, including high-tech fighters. Aircraft exterior painting is a maintenance process for long-term life management by preventing damage to the aircraft surface due to corrosion. The de-painting process is essential to ensure the quality of aircraft exterior paints. However, because the Korean Air-Force's de-painting process is currently done with sanding or Plastic Media Blasting (PMB) method, it is exposed to harmful dust and harmful compounds and consumes a lot of manpower. This study compares the de-painting process currently applied by the ROK Air-Force and the more improved process of the US Air Force, and performs economic analysis for the introduction of advanced equipment. It aims to provide information that can determine the optimal time to introduce new facilities through Cost-Volume-Profit (CVP) analysis. As a result of the analysis, it was confirmed that the sanding method had the most economical efficiency up to 2 units per year, the PMB method from 3 to 21 units, and the laser method from 22 units or more. In addition, in a situation where the amount of de-painting work is expected to increase significantly due to the increase in fighters in future, BEP analysis was conducted on the expansion of the existing PMB method and the introduction of a new laser method. As a result of the analysis, it was confirmed that it is more economical to introduce the laser method when the amount of work exceeds the PMB work capacity(18 units per year). The paper would helpful to improve the productivity and quality of the Korean Air Force Aircraft maintenance depot through timely changes of facilities in the workplace in preparation for expansion.

• 한국항공운항학회지
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• 제18권4호
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• pp.86-91
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• 2010

New Design configurations of the fighter aircraft igloo diffuser were studied based on the closed ventilation type in contrast to the conventional open distribution type. To validate the enhanced and safe performance, the exhaust flow patterns of the two igloo diffuser types were simulated by both experimental and computational approaches as design tools. Flow visualizations were conducted to investigate the exhaust flow patterns in experimental approach. In addition, the commercial code called Fluent was used to calculate flow field properties. Computational simulations provided detailed parametric studies that significantly reduced the amount of experimentation necessary to alter the design parameters of the existing fighter igloo diffuser. The closed ventilation type of the igloo diffuser was shown the better results.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 추계 학술대회논문집(수송기계편)
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• pp.53-56
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• 2005

Aircraft noise is a important problem to inhabitants near airports. INM is one of programs for determining the predicted noise impact in the vicinity of airports. It has been widely using for engineers to evaluate aircraft noise. However it is difficult to predict aircraft noise in case of lack of exact INM input data. The exact informations about a fighter plane are not known well for a security problem. This study presents methods of reducing errors between measurement and simulation when the exact INM input data is not known. Especially we adjusted the thrust force of aircraft engine and reduced the error.

• 한국소음진동공학회논문집
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• 제17권3호
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• pp.249-256
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• 2007

Aircraft noise is a serious problem to inhabitants near airports. INM is one of programs for determining the predicted noise impact in the vicinity of airports. It has been widely used for engineers to evaluate aircraft noise. However it is difficult to predict aircraft noise in case of lack of exact INM input data. The exact informations about a fighter plane are not known well for a security problem. This study presents methods of reducing errors between measurement and simulation when the exact INM input data is not known. Especially we adjusted the thrust force of aircraft engine and reduced the error.

• 제어로봇시스템학회논문지
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• 제13권1호
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• pp.6-14
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• 2007

Modem version of supersonic jet fighter aircraft must have been guaranteed appropriate controllability and stability in HAoA(High Angle of Attack). Limit value of aircraft entering into the departure in HAoA is related to aircraft configuration design. But, the control law such as AoA and yaw-rate limiter is implemented in digital Fly-By-Wire flight control system of supersonic jet fighter to guarantee the aircraft's safety in HAoA. The HAoA flight control law have two parts, one is control law of departure prevention and the other is control law of departure recovery support. The control laws of departure prevention for advanced jet trainer consist AoA limiter, roll command limiter and rudder fader. The control laws of departure recovery support are consist yaw-rate limiter and MPO(Manual Pitch Override) mode. The guideline of pitch rocking using MPO mode is simple, but operating skill of pitch rocking is very difficult by the pilot with inexperience of departure situation. This paper addresses the design and validation of APR(Automatic Pitch Rocker) control law instead of MPO in order to automatic recovery without manual pitch rocking by the pilot. And, recovery characteristic with APR verifies by the nonlinear analysis and pilot evaluation.

• 산업경영시스템학회지
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• 제45권4호
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• pp.8-20
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• 2022

The paint removal of fighter jets is just as important as the painting, because perfect paint removal ensures the quality of the exterior painting on the aircraft. However, the current conditions for paint removal work of the ROKAF's are poor. It is identified that the painting process currently implemented by the ROKAF is not only exposed to harmful compounds such as harmful dust and hexavalent chromium, but also consumes a lot of water. Thus, the introduction of advanced facility is considered. This study compares the fighter jets painting removal process currently applied by the Korean Air Force with the improved laser coating removal process of the US Air Force, and conducts an incremental analysis to perform economic analysis for the introduction of advanced facility. Four scenarios were envisioned on the premise of an increase in the number of fighters in the future, incremental analysis shows that laser coating removal method is advantageous in all scenarios. In addition, it is recommended that paint removal cycle keeps the current 12-year and the outsourcing amount to civilian depot is reduced.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1997년도 추계 학술대회논문집
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• pp.43-48
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• 1997

When computing the flow around complex three dimensional aircraft configurations, the generation of the grid is the most time consuming part. This paper presents a survey of the grid generation technique. The technique for treating problems arising in surface grid generation for complex geometries is addressed. Several example grids are shown, demonstrating the ability of the method to discretize complex geometries.