• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.9
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• pp.871-876
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• 2011

In this paper, the equilibrium flight conditions of a Korean Traditional Bangpae Kite with low aspect ratio were analyzed by it's aerodynamic data of wind tunnel test. The data of aerodynamic forces and center of pressure of the Kite were used to calculate the relative length of bridles to satisfy the condition of settling the kite to the static equilibrium steady state between ${\theta}=30^{\circ}{\sim}60^{\circ}$. From this equilibrium flight performance analysis, we obtained ($0.88{\pm}0.02$)c of the rear bridle length corresponding to 0.88c of fixed front bridle length. These results were exact agreement with the relative bridle lengths by Korean classical method.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.23 no.4
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• pp.82-88
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• 2015

Airframe maintenance is regarded the most important maintenance action in airlines as the aircraft is the most valuable asset in their operation though the volume of airframe maintenance is the last in MRO market. In the selecting process of airframe MRO provider many kinds of evaluation criteria should be considered such as quality, expenses, TAT, capability, and customer support. This paper will suggest the way to select the airframe MRO in airlines and MRO business sectors using AHP.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.9
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• pp.688-693
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• 2016

This paper describes the parachute dynamics modeling and simulation results for the development of training simulator of a HALO (High Altitude Low Opening) parachute, which is currently in use for military purposes. The target parachute is a rectangular shaped parafoil and its dynamic model is derived based on the real geometry data as the 9-DOF nonlinear equations of dynamics. The simulation was conducted through the moment of inertia and its aerodynamic derivatives to reflect the real characteristics based on the MATLAB/Simulink. In particular, its modeling includes the typical characteristics of the added mass and moment of inertia, which is shown in the strong effects in Lighter-Than-Air(LTA) flight vehicle. The proposed dynamic modeling was evaluated through the simulation under the spiral turning flight conditions of the asymmetric control inputs and compared with the performance index in the target parachute manual.

• Journal of Welding and Joining
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• v.2 no.2
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• pp.13-21
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• 1984

Chemical tanker의 Crago tank는 화학제품에 대한 내식성, 내산성 등이 요구되는 재료로서 스테인레스강이나, 스테인레스 클래드강이 주로 사용되고 있다. 이러한 스테인레스강을 사용한다 하더라도 사용시 국부적인 결함 및 부식의 문제점이 발생되고 있다. 특히 스테인레스 클래드강을 사용했을 경우 부식 및 기타 요인에 의해 결함이 발생했을 때, 클래드재(앞대기재)의 두께가 약 2.5mm 정도에 불과하므로 보수작업이 어려우며, 보수작업에 의한 산화피막의 파괴는 부식을 촉진시킨다. 이들 결함 및 부식 발생의 여러요인 중 특히 용접 시공상의 문제점이 가장 크게 영향을 미친다. 또한 용접 시공상의 문제점 중 스팻터를 제거하기 위해서는 많은 공수가 소모될 뿐 아니라 품질면에서도 나쁜 영향을 주고 있다. 본 고에서는 스팻터 생성기구의 검토와 스팻터가 모제에 미치는 영향을 다루고자 한다. 또한 용접조건 및 용접재료의 변화에 의한 스팻터 생성량 변화, 입도에 따른 비행거리 등을 검토하는데 목적을 두었다.