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- W2105296042 abstract "AbstractThe following work presents recent developments inthe simulation of helicopter rotor flows in the hoverand forward flight regimes. The simulations are car-ried out by solving the full time-accurate compress-ible flow equations, both Euler and Navier-Stokes,on a moving multiblock mesh around a rotor con-figuration. Aeroelastic effects are introduced as anintegral part of the simulation. The resulting pro-gram, ROTOR87, is implemented in parallel, using adomain decomposition approach and the MPI (Mes-sage Passing Interface) Standard for communicationpurposes. The results demonstrate that the com-bination of highly efficient algorithms and high per-formance parallel computing yields an accurate andefficient method for the computation of complex vor-tical flows of interest to the rotorcraft community.IntroductionDuring the course of the last three years, much efforthas been placed at Princeton on the development ofaccurate and efficient methods for the calculation ofunsteady viscous and inviscid flows including aeroe-lastic effects. Efficiency has been achieved throughthe use of fast implicit algorithms and the utiliza-tion of high performance parallel computing plat-forms. The pursuit of high accuracy has focusedon the implementation of refined artificial dissipa-tion algorithms which provide the necessary upwindbias without unnecessarily corrupting the flow solu-tion and the use of properly resolved meshes for thephysical phenomena at hand. It is our opinion that" @default.
- W2105296042 created "2016-06-24" @default.
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- W2105296042 date "1997-01-06" @default.
- W2105296042 modified "2023-10-14" @default.
- W2105296042 title "Time-accurate simulation of helicopter rotor flows including aeroelastic effects" @default.
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- W2105296042 doi "https://doi.org/10.2514/6.1997-399" @default.
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