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Wind Tunnel Pressure Distribution Tests on a Series of Biplane Wing Models Part I: Effects of Changes in Stagger and Gap
This report is on the changes in forces on each wing of a biplane cellule when either the stagger or the gap is varied. Since each test was carried up to a 90 degree angle of attack, the results may be used in the study of stalled flight and of spinning as well as in the structural design of biplane wings.
Date:
July 1929
Creator:
Knight, Montgomery & Noyes, Richard W.
System:
The UNT Digital Library
The Use of Wheel Brakes on Airplanes
The results of tests to determine the effect of wheel brakes on the landing run of an airplane under conditions of load and at various wind velocities are presented.
Date:
July 1929
Creator:
Carroll, Thomas & DeFrance, Smith J.
System:
The UNT Digital Library