The pressure distribution over a square wing tip on a biplane in flight

Richard V. Rhode, Eugene E. Lundquist
naca-tn-360
Jan 1931


This note presents the results obtained in pressure distribution tests on the right upper panel of a Douglas M-3 airplane in flight. These tests are a part of an extensive investigation on the effect of changes in tip shape on the load distribution.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1931/naca-tn-360.pdf