• 한국항공우주학회지
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• 제48권8호
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• pp.631-640
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• 2020

현재 항공기 시뮬레이터는 실제 항공기를 이용한 조종사 훈련에 비해 경제적, 시간적 및 공간적 비용 측면에서 상당한 이점을 가지고 있어서 많은 관심을 받고 있다. 항공기 시뮬레이터의 구성 요소 중 비행역학 모델은 실제 항공기의 비행을 모의하는데 중요한 역할을 한다. 따라서 자동화된 도구를 사용하여 비행역학 모델의 충실도를 검증하는 것은 중요한 의미를 지닌다. 본 논문에서는 항공기 시뮬레이터의 효율적인 개발을 위하여 비행역학 모델의 충실도를 자동 검증하는 소프트웨어를 개발한다. 충실도 검증 프로세스로부터 도출된 요구사항에 대하여 소프트웨어 구조 및 GUI를 설계한 다음 Window 기반 환경에서 C# 언어를 이용하여 소프트웨어를 구현한다. CTSW 기종에 대한 실험 결과는 개발된 소프트웨어가 기능 및 성능, 그리고 사용자 편의성 측면에서 효과적임을 보여준다.

• 한국항공우주학회지
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• 제37권1호
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• pp.42-54
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• 2009

비행체의 최적궤적문제에서는 최적화의 수렴성 및 효율성을 위해 3자유도 운동역학모델이 이용되며, 비선형 추종제어를 위해서는 6자유도 비선형 운동모델이 이용된다. 따라서, 3자유도 운동역학모델을 통해 획득한 최적궤적을 비선형 추종제어의 기준궤적으로 사용하는 경우에 두 모델간의 상이성으로 인한 문제가 발생하게 되며 성능이 보장하지 못한다. 본 논문에서는 이러한 두 모델간의 차이를 완화시키기 위한 새로운 최적궤적 생성 방법을 제안하였으며, 성층권비행선의 실제 구속조건과 성능조건 및 제트 스트림을 고려하여 최적궤적을 생성하고 기존 결과와 비교함으로써 제안한 방법의 장점을 검증하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.167-171
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• 2012

비행고도가 우주비행체 자세제어용 하이드라진 추력기 노즐의 추력성능 특성에 미치는 영향을 규명하기 위해 노즐유동 해석을 수행한다. k-${\omega}$ SST 난류모델을 사용한 Reynolds-averaged Navier-Stokes 방정식으로 노즐유동을 비행고도 변이별로 해석하되, 비행고도는 연속체역학이 유효한 범위내로 제한한다. 작동 고도가 10 km 이하일 때는 노즐내부에 충격파 및 유동박리 등의 비가역적 현상이 발생하여 추력성능이 감소하였으나, 30 km 이상의 고도환경에서는 공칭추력 수준으로 회복되었다.

• 한국항공운항학회지
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• 제16권3호
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• pp.15-20
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• 2008

At the choice of aviation company, safety appears as biggest variable than expenses, speed and comfort so these are concerned not only aviation companies but also countries and customers. Until now, ICAO has been making effort to reduce the flight accident through the safety advice of aviation part, establishment of standard, education, training and develop of navigation aids. Especially in 2008, they emphasize that the flight accident is reduced through researches and applications about SMS as safety regulation. Important primary factor to give influence about promotion of SMS is practice of organization and for this, to investigate recognition about safety management and culture of members. At point of this, this research analyze the recognition degree about how to manage safety and SMS for pilots an mechanics of Korea.

• Advances in aircraft and spacecraft science
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• 제9권1호
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• pp.17-37
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• 2022

This paper discusses an improved unmanned aerial vehicle, UAV, configuration characterized by telescopic booms to optimize the flight mechanics and fuel consumption of the aircraft at various loading/flight conditions.The starting point consists of a full-composite smaller UAV which was derived by a general aviation ultralight motorized aircraft ULM. The present design, named ToBoFlex, extends the two-booms configuration to a three tons aircraft. To adapt the design to needs relevant to different applications, new solutions were proposed in aerodynamic fields and materials and structural areas. Different structural solutions were reported. To optimize aircraft endurance, the innovative concept of Telescopic Tail Boom was considered along with two different tails architecture. A new structural configuration of the fuselage was proposed. Further consideration of hydrogen fuel cell electric propulsion is now being studied in collaboration between the Polytechnic of Turin and Prince Mohammad Bin Fahd University which could be the starting point of future investigations.

• Structural Engineering and Mechanics
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• 제20권5호
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• pp.575-587
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• 2005

Using the nonlinear load transfer function for pile side soil and the linear load transfer function for pile end soil, a combined approach of the incremental load transfer matrix method and the approximate differential equation solution method is presented for the nonlinear analysis of interaction between flexible pile group and soil. The proposed method provides an effective approach for the solution of the nonlinear interaction between flexible pile group under rigid platform and surrounding soil. To verify the accuracy of the proposed method, a static load test for a nine-pile group under a rigid platform is carried out. The finite element analysis is also conducted for comparison purposes. It is found that the results from the proposed method match very well with those from the experimental test and are better in comparison with the finite element method.

• 항공우주의학회지
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• 제30권2호
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• pp.61-65
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• 2020

In the case of aviation maintenance work, several kinds of shift works are performed during day and night, and a lot of works are performed on the ramp due to the characteristics of the aircraft flight schedule. Maintenance workers are often exposed to the sun or in cold temperatures for aircraft maintenance works. The fatigue risk of the maintenance workers will be weighted. In particular, the work at night shift under normal biological rhythms can make maintenance workers feel sleepy during daytime work. It can also affect the safety of aircraft and individual workers. Accordingly, this study will consider fatigue-related previous researches in the field of aviation maintenance, review the effects of shift work, and how fatigue affects aviation mechanics during the day/night shifts. Considering these factors, we tried to present a plan that can minimize the fatigue of aviation workers through this study.

• Advances in aircraft and spacecraft science
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• 제10권2호
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• pp.107-125
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• 2023

Drag reduction is significant research in aircraft design due to its effect on the cost of operation and carbon footprint reduction. Aircraft currently use conventional solid winglets to reduce the induced drag, adding extra structural weight. Fluidic on-demand winglets can effectively reduce drag for low-speed flight regimes without adding any extra weight. These utilize the spanwise airflow from the wingtips using hydraulic actuators to create jets that negate tip vortices. This study develops a computational model to investigate fluidic on-demand winglets. The well-validated computational model is applied to investigate the effect of injection velocity and angle on the aerodynamic coefficients of a rectangular wing. Further, the turbulence parameters such as turbulent kinetic energy (TKE) and turbulent dissipation rate are studied in detail at various velocity injections and at an angle of 30°. The results show that the increase in injection velocity shifted the vortex core away from the wing tip and the increase in injection angle shifted the vortex core in the vertical direction. Further, it was found that a 30° injection is efficient among all injection velocities and highly efficient at a velocity ratio of 3. This technology can be adopted in any aircraft, effectively working at various angles of attack. The culmination of this study is that the implementation of fluidic winglets leads to a significant reduction in drag at low speeds for low aspect ratio wings.

• 한국항행학회논문지
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• 제28권4호
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• pp.524-531
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• 2024

글로벌 환경에서 항공사는 고객 만족을 통해 경쟁력을 확보하고 이윤을 창출하기 위해 노력하고 있다. 고객에게 서비스를 제공하기 위해 가장 선행되어야 할 것이 항공기의 안전이며, 안전의 실현을 위해 기본이 되어야 할 것이 정비품질의 지속적 유지이다. 항공 기술의 발전 정도는 상상할 수 없을 만큼 빠르게 진행되고 있으나, 정비품질 유지를 위해 일선 현장에서 업무하는 항공정비사의 제반 환경은 크게 변함이 없는 실정이다. 본 연구에서는 항공정비사에게 제공되는 교육훈련과 안전문화의 수준을 파악하고 자아존중감이 정비품질에 미치는 영향을 알아보고자 한다. 기존 선행연구는 정비사의 교육훈련, 조직성과 ,직무스트레스 등과 같은 연구는 있었으나, 정비품질과 관련된 연구는 부족하였다. 따라서 본 연구는 정비품질에 영향을 미치는 변수 간의 관계를 파악하고 실증분석을 통한 정비품질 향상을 위한 시사점을 제시하고자 한다.

• Earthquakes and Structures
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• 제9권2호
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• pp.375-390
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• 2015

Staircase is a vertical transportation element commonly used in every multistoried structure. Inclined flights of staircase are usually casted monolithically with RC frame. The structural configuration of stairs generally introduces discontinuities into the typical regular reinforced concrete frame composed of beams and columns. Inclined position of flight transfers both vertical as well as horizontal forces in the frame. Under lateral loading, staircase in a multistory RC frame building develops truss action creating a local stiffening effect. In case of seismic event the stiff area around staircase attracts larger force. Therefore, special attention is required while modeling and analyzing the building with staircase. However, in general design practice, designers usually ignore the staircase while modeling either due to ignorance or to avoid complexity. A numerical study has been conducted to examine the effect of ignoring staircase in modeling and design of RC frame buildings while they are really present in structure, may be at different locations. Linear dynamic analysis is performed on nine separate building models to evaluate influence of staircase on dynamic characteristics of building, followed by nonlinear static analysis on the same models to access their seismic performance. It is observed that effect of ignoring staircase in modeling is severe and leads to unsafe structure. Effect of location and orientation of staircase is also important in determining seismic performance of RC frame buildings.