NASA NTRS · 19930080947
The induction factor used for computing the rolling moment due to the ailerons
Abstract
In the following note, prepared for the National Advisory Committee for Aeronautics, this induction factor is determined from the result of a model test, and compared with a formula recently developed by the author. The two results are found to be in substantial agreement.
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Munk, Max M. 1924-04-01. The induction factor used for computing the rolling moment due to the ailerons. https://ntrs.nasa.gov/citations/19930080947
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