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- W2367779670 abstract "The experimental investigation conducted in CARDC Dia. 3.2m subs onic wind tunnel for a fighter model with 57° delta wing are presented and the t ypical results are also discussed in this paper. During the test forces and mome nts are measured under pitching, yawing and rolling oscillation with the amplitu de of 20°,35° and reduced frequency from 0 to 0.2 at various side slip and ang les of attack for longitudinal and lateral motion respectively. On the basis of Fourier functional analysis and the linear aerodynamic theories，two aerodynami c models were built up.The calculated results with the models,the Fourier analys is model and the nonlinear model, show good agreement between different methods and test results." @default.
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- W2367779670 date "2000-01-01" @default.
- W2367779670 modified "2023-09-25" @default.
- W2367779670 title "An experimental investigation on unsteady aerodynamics and modeling for a fighter configuration" @default.
- W2367779670 hasPublicationYear "2000" @default.
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