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- W346021434 abstract "A new method is presented for using Navier-Stokes results in the system analysis and sensitivity derivative computations for a helicopter rotor in hover. The system coupling includes the interactions between rotor performance, rotor structural properties and aerodynamics (i.e., airfoil shape). Emphasis is placed on the use of high fidelity Navier-Stokes algorithms for the aerodynamic problem. The present formulation is chosen to reduce the number of sensitivity derivative equations and their dimensions as much as possible. In addition, an alternative adjoint formulation is presented which dramatically reduces the computational requirement for disciplines in which there may be a large number of design variables (e.g., aerodynamics). The theoretical method makes use of a combination of derivatives from each discipline; the computation of these derivatives has already been shown to be feasible. Sample computations for the aerodynamic-rotor model coupling and an associated sensitivity derivative are also presented." @default.
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- W346021434 date "1992-08-17" @default.
- W346021434 modified "2023-09-26" @default.
- W346021434 title "Multidisciplinary analysis and sensitivity derivatives for isolated helicopter rotors in hover" @default.
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- W346021434 doi "https://doi.org/10.2514/6.1992-4696" @default.
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