• 한국항공우주학회지
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• 제35권11호
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• pp.983-989
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• 2007

위그선(WIG: Wing In Ground effect)은 해수면상의 저고도에서 운영되기 때문에 조류충돌에 쉽게 노출될 수 있으며 특히 리딩에지(Leading Edge)는 충돌가능성이 높기 때문에 조류충돌에 대한 구조적 안정성 검증과정이 반드시 필요하다. 이러한 항공기에 대한 조류충돌은 매우 복잡한 현상중의 하나로 다양하고 불확실한 파라메터들이 존재한다. 조류충돌에 대한 해석과정에 있어서 불확실성이 존재하는 파라메터들이 충돌 해석결과에 미치는 영향력을 분석하기 위해 퍼지이론을 적용한 유한요소 해석을 수행하였다. 불확실한 파라메터들이 갖는 조류충돌에 대한 영향력은 비선형 충돌해석 프로그램인 LS-DYNA 3D를 사용하여 해석하였으며 조류충돌 현상에 존재하는 다양하고 불확실한 파라메터들은 퍼지숫자(Fuzzy number)와 멤버십 함수(Membership function)로 표현하여 퍼지연산 및 변환기법(Transformation method)을 통해 해석과정에 적용하였다. 결론적으로 불확실성이 존재하는 파라메터들이 조류충돌 현상에 미치는 영향력을 퍼지 연산을 통해 수치적으로 평가하였다.

• Restorative Dentistry and Endodontics
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• 제9권1호
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• pp.81-87
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• 1983

The purpose of this study was to observe and identify the phases of amalgam and to know the transformation of microstructure in the set amalgam by lapse of time. In this study, shofu spherical-D alloy was used. After trituration of amalgam alloy and mercury (Wig-L-Bug), it was filled in the stone dies. This specimens being polished and etched by usual method was observed under optical microscope using metallurgical microscope. And then X-ray diffractometer was used to analyze the phases contents and transformation of microstructure at $2{\frac{1}{2}}$ hours, 15 hours, 28 hours and 2 years after being amalgamated. The following results were obtained: 1. Shofu spherical-D alloy powder was composed of ${\gamma}$ phase, ${\epsilon}$phase and Ag-Cu eutectic phases. 2. ${\gamma}_2$ phases were appeared at $2{\theta}$ values ($32.0^{\circ}$ and $43.8^{\circ}$) in the amalgam which was analyzed at $2{\frac{1}{2}}$ hours and 15 hours after trituration with mercury. 3. In the amalgam at 28 hours, ${\gamma}_2$ phase was found at $2{\theta}$ value ($43.8^{\circ}$) at 35 hour, $r_2$ phase was appeared at $2{\theta}$ value $32.0^{\circ}$. 4. No ${\gamma}_2$ phases were observed in the 2 years old amalgam. But ${\eta}$ ($Cu_6Sn_5$) phases were found at $2{\eta}$ values $29.4^{\circ}$ and $42.4^{\circ}$.