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- W2085146070 abstract "This paper presents an overview of a joint Experimental/Numerical project sponsored by the Swedish Defense Materiel Administration (FMV) to apply flow control techniques to reduce the noise from high-performance military aircraft such as the Saab Gripen. At University of Cincinnati chevrons and trailing-edge fluidic injection were tested and compared with secondary flow simulating forward flight. At Chalmers University the same conditions were simulated with Large Eddy Simulation and Kirchhoff integral method. Both flow control approaches produced significant reductions in community noise. The area for a given peak perceived noise level was reduced by 20-27% by chevrons and by 23-38% by microjets." @default.
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- W2085146070 date "2010-06-07" @default.
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- W2085146070 title "Comparison of Flow Control Methods Applied to Conical C-D Nozzles" @default.
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- W2085146070 doi "https://doi.org/10.2514/6.2010-3874" @default.
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