Air force and three moments for F-5-L Seaplane

Aeronautics Staff, Construction Department, Navy Yard, Washington, D.C.
naca-tn-85
February, 1922


A model of the F-5-L seaplane was made, verified, and tested at 40 miles an hour in the 8' x 8' tunnel for lift and drag, also for pitching, yawing and rolling moments. Subsequently, the yawing moment test was repeated with a modified fin. The results are reported without VL scale correction.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1922/naca-tn-85.pdf