Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 14. Errata and Revisions

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Report Number: AF TR 5761 Part 14
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-11-01
Pages: 35
Contract: W33-038-ac-16961
DoD Task:
Identifier: AD0089717

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Provenance: Bombardier/Aero

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