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- W2321817805 abstract "The twist shapes adopted by wind tunnel model wings under tunnel loads can have a significant effect on the vortex drag levels measured for typical airliner designs, yet are difficult to predict theoretically or to measure experimentally. The problem of accurately determining model twist shapes becomes particularly important when tests are performed in pressurised test facilities, which typically feature large wind-off to wind-on wing twist changes. In such tests, percentage twist errors which would be negligibly small in atmospheric testing can be magnified to a point where they have a marked effect on aerodynamic force measurements. This paper describes work recently performed at Airbus UK to determine the twist shapes adopted by a research model wing at a range of test conditions in the European Transonic Windtunnel (ETW). The task involved developing a finite element model incorporating a simplified representation of the model wing's internal structure, then validating it against data from a series of bench tests performed on the tunnel model. The validated finite element model has since been used to calculate the shape of the wing at a range of test conditions encountered during testing within the EU Fifth Framework programme HiReTT. It has also demonstrated the accuracy of the methodology used by Airbus UK to define the build shape of wind tunnel models." @default.
- W2321817805 created "2016-06-24" @default.
- W2321817805 creator A5041083103 @default.
- W2321817805 date "2002-01-14" @default.
- W2321817805 modified "2023-09-27" @default.
- W2321817805 title "Investigation of wind tunnel model deformation under high Reynolds number aerodynamic loading" @default.
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- W2321817805 doi "https://doi.org/10.2514/6.2002-424" @default.
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