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- W2032259318 abstract "Methods are presented for representing unsteady aerodynamic loadings, valid for arbitrary motion, for the two-dimensional typical section with a trailing-edge control surface in incompressible flow and a three-dimensional lifting surface with leading- or trailing-edge control surfaces in subsonic compressible flow. Loads for the two-dimensional incompressible case are obtained via analytic continuation of the Theodorsen function into the complex plane, with guidance from a time-domain approximation of the Wagner indicial function. For the three-dimensional case, it is proposed that oscillatory generalized aerodynamic forces be approximated by Pade fractions, thereby permitting an obvious continuation into the complex plane. A theoretical justification for this procedure is briefly outlined, and some practical aspects of its implementation are discussed." @default.
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- W2032259318 date "1973-08-16" @default.
- W2032259318 modified "2023-09-25" @default.
- W2032259318 title "Control law synthesis and sensor design for active flutter suppression" @default.
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- W2032259318 doi "https://doi.org/10.2514/6.1973-832" @default.
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