The induction factor used for computing the rolling moment due to the ailerons

Max M. Munk
naca-tn-187
April, 1924


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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1924/naca-tn-187.pdf