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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
Author(s): Williams, M. L., Garrett, J., Henry, W. E.Corporate Author(s): Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1950-11-01
Report number: AF TR 5761 Part 7
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