Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 3. Experimental Investigation of the Effect of Sweep Upon the Stress and Deflection Distribution in Cantilever Plates of Constant Chord and Thickness

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Report Number: AF TR 5761 Part 3
Author(s): DeGroff, Harold M.
Corporate Author(s): Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1950-10-01
Pages: 136
Contract: W33-038-ac-16961
DoD Task:
Identifier: AD0089758

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Provenance: Bombardier/Aero

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