Comparison of experimental with calculated results for the lifting effectiveness of a flexible 45 degree sweptback wing of aspect ratio 6.0 at Mach numbers from 0.8 to 1.3

Richard E. Walters
Apr 1954

Tests were conducted on models having 45 degree sweptback wings with varying degrees of flexibility to determine the effective lift-curve slopes in order to evaluate the usefulness of a general method for the prediction of the effective lift ratio by a comparison of the predicted values with the test results.

An Adobe Acrobat (PDF) file of the entire report: