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Theoretical and Experimental Effect of Sweep upon Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 2. Stress and Deflection Analysis of Swept Plates
Author(s): Fung, Yung-Cheng
Corporate Author(s): Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1949-12-01
Report number: AF TR 5761 Part 2

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