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공력 향상과 RCS 감소를 고려한 무인 전투기의 형상 최적설계
조영민(Y.M. Jo),최성임(S.I. Choi) 한국전산유체공학회 2011 한국전산유체공학회 학술대회논문집 Vol.2011 No.11
Nowadays, Unmanned Combat Air Vehicle(UCAV) has become an important aircraft system for the national defense. For its efficiency and survivability, shape optimization of UCAV is an essential part of its design process. In this paper, shape optimization of UCAV was processed for aerodynamic performance improvement and Radar Cross Section(RCS) reduction using Multi Objective Genetic Algorithm(MOGA). Lift and induced drag, friction drag, RCS were calculated using panel method, boundary layer theory, Physical Optics(PO) approximation respectively. In particular, calculation applied Radar Absorbing Material(RAM) was performed for the additional RCS reduction. Results are indicated that shape optimization is performed well for improving aerodynamic performance, reducing RCS. further study will be performed with higher fidelity tools and consider other design segments including structure.
공력 향상과 RCS 감소를 고려한 무인 전투기의 형상 최적설계
조영민(Y.M. Jo),최성임(S.I. Choi) 한국전산유체공학회 2012 한국전산유체공학회지 Vol.17 No.4
Nowadays, Unmanned Combat Air Vehicle(UCAV) has become an important aircraft system for the national defense. For its efficiency and survivability, shape optimization of UCAV is an essential part of its design process. In this paper, shape optimization of UCAV was processed for aerodynamic performance improvement and Radar Cross Section(RCS) reduction using Multi Objective Genetic Algorithm(MOGA). Lift and induced drag, friction drag, RCS were calculated using panel method, boundary layer theory, Physical Optics(PO) approximation respectively. In particular, calculation applied Radar Absorbing Material(RAM) was performed for the additional RCS reduction. Results are indicated that shape optimization is performed well for improving aerodynamic performance, reducing RCS. Further study will be performed with higher fidelity tools and consider other design segments including structure.
유동 간섭 효과를 고려한 Wing-sails 공력 최적 설계
이학진(H.J. Lee),조영민(Y.M. Jo),권형일(H.I. Kwon),최성임(S.I. Choi) 한국전산유체공학회 2013 한국전산유체공학회 학술대회논문집 Vol.2013 No.5
These day, an issues related with environments are becoming more pressing. We investigated potential next-generation vessel which makes use of the wing-sails to support existing fossil fuel-based propulsion system. The sailing-ship is a new concept eco-friendly vessel that uses the wind energy to produce additional thrust force by wing-sails above the hull. In this study, we focused on the aerodynamic analysis and design optimization of multiple wing-sails by varying the wind direction 15 degrees to 165 degrees. For the numerical analysis, we solved three dimensional compressible Navier-stokes equation with Spalart-Allmaras turbulent model. After the investigation of aerodynamic characteristics around wing-sails and the effect of flow interactions, we performed the design optimization of wing-sails by considering both single wing-sail and multiple wing-sails. In single wing-sail design, we found optimal value of deflection angle and flap length of single wing-sail to maximize the lift performance. In multiple wing-sails design, we carried out design optimization to find an optimal set-up of individual for each of the wing-sails that maximize total thrust of wing-sails. These optimal set-up include a deflection angle, deflection length and angle of attack of each wing-sails. Using a Kriging-based surrogate model and the derivative-free optimization method of genetic algorithms (GAs), we found the optimal set-up of the single and multiple wing-sails. The design optimization results showed that the total thrust of wing-sails has improved by 27~36% corresponding to the varying the wind directions.
e-Science 기반 EDISON 포탈의 항공우주분야 에어포일 공력 최적 설계 프레임워크 개발
권형일(H.I. Kwon),조영민(Y.M. Jo),이슬기(S.G. Yi),김사지(S.J. Kim),최성임(S.I. Choi) 한국전산유체공학회 2012 한국전산유체공학회 학술대회논문집 Vol.2012 No.5
Design optimization is to find optimum of design space which is defined by design variables, using optimization algorithm. Recently, numerical design optimization including computational fluid dynamics (CFD) has been focused in not only aerospace engineering, but general engineering field because of many research and development for high performance computing. However it could hardly find the design optimization softwares and contents of which educational or research purposes in aerospace engineering. In this study, as one framework of EDISON DESIGN OPTIMIZATION, aerodynamic design optimization framework for an airfoil based on EDISON (EDucation-research Integration through Simulation On the Net) portal. As well as the softwares development, essential contents are also developed for the lecture associated with design optimization in the aerospace engineering. Software and contents on aerodynamic design optimization could be expected to be assisted in the lecture or lab..
이학진(H.J. Lee),조영민(Y.M. Jo),최성임(S.I. Choi),권종오(J.O. Kwon),안성목(S.M. Ahn) 한국전산유체공학회 2012 한국전산유체공학회 학술대회논문집 Vol.2012 No.11
The sailing ship is a eco-friendly vessels that using wind energy to produce the additional thrust by the hull above the wing-sails. In this study, we performed the aerodynamic analysis around wing-sails by considering the interaction of wing-sails in fixed angle of attack. The wind direction that produces the maximum thrust of wing-sails can be obtained by calculating the thrust of wing-sails with, respect to the wind direction. In the aerodynamic analysis, we used three-dimensional compressible Navier-Stokes equation and hybrid grid to predict more viscous flow of boundary layer. We investigated that the maximum thrust of wing-sails at wind direction of 90 degree. After studying on the flow characteristic around wing-sails and effect of interaction, through derivative free based genetic algorithm and kriging surrogate model method to substitute a objective function evaluation we searched the optimal angle of attack that maximize the thrust of wing-sails. The result of optimization about wind direction of 45, 90 and 135 degree, we acquired about 7~23% of trust increment with trend of increasing the rear wing-sailss angle of attack by the interaction of wing-sails. Also we confirmed the thrust enhancement of 2~18% by conducting a three-dimensional validation.