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- W1989192011 abstract "Full-scale wind-tunnel tests, conducted to determine the effects of three different airfoil sections on the aft-fuselage drag of a low-wing aircraft, are described. The measurements indicate a maximum difference in aft fuselage drag between the three airfoils of about 0.002. Measured changes in the locations of the fuselage pressure contours with airfoil section correlated well with the changes predicted by a three dimensional paneling code. A criterion, based on the inviscid computer code, is then proposed as an indicator for possible adverse viscous interactions at the wing-fuselage juncture." @default.
- W1989192011 created "2016-06-24" @default.
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- W1989192011 date "1981-08-11" @default.
- W1989192011 modified "2023-09-24" @default.
- W1989192011 title "Full-scale wind-tunnel study of wing-fuselage interaction and comparison with paneling method" @default.
- W1989192011 doi "https://doi.org/10.2514/6.1981-1666" @default.
- W1989192011 hasPublicationYear "1981" @default.
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