ESDU 08013
Increment in wing profile drag coefficient due to the deployment of a single-slotted flap.
Abstract:
ESDU 08013 provides an empirical method for predicting the wing profile drag coefficient increment due to the deployment of a single-slotted flap. The estimate is intended for use within the estimate of thelow-speed drag polar of a wing with deflected flap. The estimate includes a lift-dependent component.
Comparisons with experimental data demonstrate the accuracy of the method. The method applies to wings of moderate to high aspect ratio and modest sweep. Worked examples illustrate the use of the method.
A program of the method is provided as Toolbox 08013 and ESDUpac A0813.
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This Data Item is complemented by the following software:
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08013 Toolbox
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ESDUpac A0813 New in this Release
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This program is only available to subscribers. |