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Performance Evaluation of Two-Equation Turbulence Models for 3D Wing-Body Configuration
곽인근,이남훈,이승수,박상일 한국항공우주학회 2012 International Journal of Aeronautical and Space Sc Vol.13 No.3
Numerical simulations of 3D aircraft configurations are performed in order to understand the effects of turbulence models on the prediction of aircraft's aerodynamic characteristics. An in-house CFD code that solves 3D RANS equations and two-equation turbulence model equations are used. The code applies Roe’s approximated Riemann solver and an AF-ADI scheme. Van Leer’s MUSCL extrapolation with van Albada’s limiter is also adopted. Various versions of Menter’s k-ω SST turbulence models as well as Coakley’s q-ω model are incorporated into the CFD code. Menter’s k-ω SST models include the standard model, the 2003model, the model incorporating the vorticity source term, and the model containing controlled decay. Turbulent flows over a wing are simulated in order to validate the turbulence models contained in the CFD code. The results from these simulations are then compared with computational results from the 3rd AIAA CFD Drag Prediction Workshop. Numerical simulations of the DLR-F6 wing-body and wing-body-nacelle-pylon configurations are conducted and compared with computational results of the 2nd AIAA CFD Drag Prediction Workshop. Aerodynamic characteristics as well as flow features are scrutinized with respect to the turbulence models. The results obtained from each simulation incorporating Menter’s k-ω SST turbulence model variations are compared with one another.
박상일(Sang-Il Park),곽인근(Einkeun Kwak),이승수(Seungsoo Lee) 한국항공우주학회 2011 韓國航空宇宙學會誌 Vol.39 No.4
본 논문에서는 항공기의 항력 감소를 위해 페어링 형상을 설계하고 설계 형상에 대한 공력해석을 수행하였다. 페어링은 날개 끝과 날개-동체 접합부에 대해 적용되었다. 날개 끝 페어링의 경우 날개 천체에 대한 유동 해석을 수행하였고 날개-동체 페어링에 대해서는 전기체에 대한 해석을 수행하였다. Menter의 κ-ω SST 난류 모델이 적용된 3차원 RANS 코드를 이용하였으며 유동 해석을 실시하였다. 페어링의 형상과 유무에 따른 해석 결과를 비교하여 각각의 페어링 날개와 항공기의 항력에 미치는 영향을 확인하였다. In this study, fairing configurations for an aircraft are designed and the aerodynamic analyses of the fairings are performed to find the best choice for the aircraft. Fairings considered are wing-tip fairing and wing-body fairing. Wing alone analyses are done for the wing-tip faring selection, while wing-body-tail analyses are done for the wing-body fairing selection. A 3-D RANS solver with Menter's κ-ω SST turbulence model are used for the aerodynamic analyses. The effects on the drag of the aircraft are examined by comparing the analysis results with and without the farings.