• 한국수학교육학회지시리즈E:수학교육논문집
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• 제22권4호
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• pp.505-514
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• 2008

방정식의 가해성 탐구는 수학사의 중요한 연구주제의 하나였으며, 삼차방정식과 사차방정식의 일반적인 해법은 교사양성기관의 현대대수학 교과에서 다루는 중요한 내용이다. 본 연구에서는 norm형식의 개념을 바탕으로 이차방정식의 근의 공식에 대한 방법유추를 통해 삼차방정식의 근의 공식을 유도하고, 삼차방정식의 근의 공식에 대한 방법유추를 통해 사차방정식의 근의 공식을 유도하였다.

• 소음진동
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• 제6권5호
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• pp.607-616
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• 1996

A combined computational fluid dynamics(CFD)-Kirchhoff method is presented for predicting high-speed impulsive noise generated by a hovering blade. Two types of Kirchhoff integral formula are used; one for the classical linear Kirchhoff formulation and the other for the nonlinear Kirchhoff formulation. An Euler finite difference solver is solved first to obtain the flow field close to the blade, and then this flow field is used as an input to a Kirchhoff formulation to predict the acoustic far-field. These formulas are used at Mach numbers of 0.90 and 0.95 to investigate the effectiveness of the linear and nonlinear Kirchhoff formulas for delocalized flow. During these calculiations, the retarded time equation is also carefully examined, in particular, for the cases of the control surface located outside of the sonic cylinder, where multiple roots are obtained. Predicted results of acoustic far-field pressure with the linear Kirchhoff formulation agree well with experimental data when the control surface is at the certain location(R=1.46), but the correlation is getting worse before or after this specific location of the control surface due to the delocalized nonlinear aerodynamic flow field. Calculations based on the nonlinear Kirchhoff equation using a linear sonic cylinder as a control surface show a reasonable agreement with experimental data in negative amplitudes for both tip Mach numbers of 0.90 and 0.95, except some computational integration problems over a shock. This concliudes that a nonlinear formulation is necessary if the control surface is close to the blade and the flow is delocalized.