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논문 기본 정보

자료유형
학술저널
저자정보
Yue Kuizhi (Naval Aeronautical and Astronautical University) Chen ShiChun (Beijing University of Aeronautics and Astronautics) Liu Wenlin (Naval Aeronautical and Astronautical University) Yu Dazhao (Naval Aeronautical and Astronautical University)
저널정보
한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.15 Number.4
발행연도
2014.12
수록면
366 - 373 (8page)

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초록· 키워드

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A conceptual design of a three-surface strike fighter was studied and stealth performance was taken into account to enhance survivability and battle effectiveness. CATIA was used to design the aircraft’s three-dimensional prototype model and the weapon carriage arrangement was also studied. The aircraft’s RCS characteristics and distributions under X, S, C, and L bands were simulated using the RCSPlus software, which is based on the PO method. Pressure and velocity distributions of the flow field were also simulated using CFD. A turbulence model was based on standard k-ε function and N-S functions were used during the CFD computation. Lift coefficients, drag coefficients, and lift-to-drag ratio were obtained by aerodynamic simulation. The results showed that: (1) the average value of head-on RCS between ±30° is below -3.197 ㏈sm, and (2) the lift coefficient is 0.34674, the drag coefficient is 0.04275, and the lift-to-drag ratio is 8.11087 when the attack angle is 2.5°.

목차

Abstract
1. Introduction
2. Theoretical Basis
3. Aircraft Conceptual Design
4. Simulation
5. Conclusions
References

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UCI(KEPA) : I410-ECN-0101-2016-558-000990512