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- W1993164310 abstract "The use of tail strakes on aft loading transport aircraft is a well proven technique to reduce fuselage upsweep drag. In the present paper the tail flow around a generic aircraft configuration with a swept up tail has been computed using high fidelity CFD analyses. The focus was on the influence and effectiveness of tail strakes and the interaction of the strake with the tail vortices. As it turned out that strakes placed arbitrarily may lead to decrease of aircraft performance, CFD based optimization runs were conducted to find an optimal strake position on the rear fuselage. Finally the optimized configurations were analyzed and the principle of strake tail vortex interaction aiming on a reduction of upsweep drag was clarified." @default.
- W1993164310 created "2016-06-24" @default.
- W1993164310 creator A5015511620 @default.
- W1993164310 date "2010-06-28" @default.
- W1993164310 modified "2023-10-05" @default.
- W1993164310 title "Investigation and Minimization of Upsweep Drag of Aft-Loading Military Transporters with Tail Strakes" @default.
- W1993164310 cites W2276819466 @default.
- W1993164310 doi "https://doi.org/10.2514/6.2010-4365" @default.
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