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- W2067043112 abstract "This paper presents the application of the CANARI flow solver to the computation of unsteady effects in the aerodynamic interaction of a high speed propeller with the aircraft. The method is first validated on the APIAN isolated propeller test case by comparison with experiment at M=0.7. The method is then applied to the time accurate 3D Euler computation of a generic transport aircraft at M=0.68. Analysis of the results shows significant unsteady effects both on the propeller forces and on the wing aerodynamic flows, by comparison with steady computations." @default.
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- W2067043112 date "2003-09-01" @default.
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- W2067043112 title "Improvements on computations of high speed propeller unsteady aerodynamics" @default.
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- W2067043112 doi "https://doi.org/10.1016/s1270-9638(03)00046-4" @default.
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