THEORETICAL AND EXPERIMENTAL EFFECT OF SWEEP UPON THE STRESS AND DEFLECTION DISTRIBUTION IN AIRCRAFT WINGS OF HIGH SOLIDITY Part 7. An Experimental Investigation of the Stresses and Deflections in a Series of Cantilever Sectors of Uniform Thickness

摘要

This report deals with the deflections of sectors of uniform thickness from the standpoint of experimentally determined influence coefficients. A family of sectors having opening angles ranging from 30 to 180 degrees will be considered.