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- W2361492066 abstract "The transonic flows at high angle of attack around a twin-tail complete fighter configurationhave been numerically simulated with a two-equation model k-g,which was derived from model k-ω.Model k-g,because of such advantages as no use of normal-to-wall distance,simple source terms andvery straightforward boundary conditions,can be easily extended to practical and complex configurations.According to the geometric characteristics of the fighter,three-block structured grids with point-to-point boundaries are generated by combination of algebraic and solving elliptic equation methods.On thebasis of multi-block mesh system,zonal method is employed to solve the equations of k-g model and themean flow.Concretely,the equations of model k-g are explicitly integrated similarly as the Reynolds av-eraged Navier-Stokes equations with central-differencing and artificial dissipation for each sub-zone.Thesimilar transonic flows at high angle of attack around the NASA TN D-712 standard wing-fuselage mod-el are used to validate the codes.The computational results are compared to available experiment dataand good agreement is achieved.At the same time,another wide-used turbulence model,the algebraicBaldwin-Lomax model,is also applied for these viscous flows." @default.
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- W2361492066 date "2006-01-01" @default.
- W2361492066 modified "2023-09-23" @default.
- W2361492066 title "Numerical simulation for transonic flows at high incidence around a complete fighter with two-equation k-g model" @default.
- W2361492066 hasPublicationYear "2006" @default.
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