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- W960076009 abstract "Due to their advantages in aerodynamic characteristics, delta-canard configurations (Figure 1) have experienced growing interest and have been realized in various recent aircraft designs. Aerodynamic modeling and identification of parameters of these configurations have been usually restricted to the constant and linear terms in a Taylor series approximation of the force and moment coefficients. These modeling approaches are straight-forward and easy to handle in parameter identification processes but sometimes lack physical understanding of the flow phenomena. The present work extends those models by nonlinear and higher order terms. Emphasis is put on the objective to be able to explain and justify those model extensions by physical background." @default.
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- W960076009 date "1997-07-01" @default.
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- W960076009 title "Elements of Aerodynamic Model Validation for Delta-Canard Configured Aircraft with Thrust-Vectoring" @default.
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- W960076009 doi "https://doi.org/10.1016/s1474-6670(17)42879-5" @default.
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