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
naca-rm-l54b16
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.

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http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-l54b16.pdf