On a kernel-function method for the calculation of pressure distributions on wings with harmonically oscillating control surfaces in subsonic flow

Report (1971)

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Published Date

03-08-1971

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NLR TR 70123 U

Abstract

Local solutions for the pressure distribution at the leading and side edges of harmonically oscillating unbalanced control surfaces have been fitted into an existing lifting surface method for wings without control surfaces. Calculated results are compared with results of other methods and with experiments.

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