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- W2328296411 abstract "The AIAA Applied Aerodynamics Technical Committee’s Rotorcraft Simulation Working Group put together standardized evaluation of the S-76 planform in hover. The objective of this paper was to construct a hybrid analysis framework for the baseline S-76 planform and compute performance predictions for various collective settings and compare with experiments. The hybrid method consists of a near-body rotor-blade Navier-Stokes solver coupled with a farfield Lagrangian wake evolution model. Apart from thrust, torque coefficients and rotor figure of merit, the computed wake structure and surface pressure distributions are also obtained. The paper concludes with some observations on the suitability of hybrid methods for hover computation. Nomenclature μ advance ratio Cp power coefficient CT rotor thrust coefficient FM figure of merit αs shaft angle of attack σ solidity CnM 2 sectional normal loads CmM 2 sectional pitching moments" @default.
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- W2328296411 date "2014-01-10" @default.
- W2328296411 modified "2023-10-17" @default.
- W2328296411 title "Analysis of a Rotor in Hover using Hybrid Methodology" @default.
- W2328296411 doi "https://doi.org/10.2514/6.2014-0210" @default.
- W2328296411 hasPublicationYear "2014" @default.
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