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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 6. The Plate Problem for a Cantilever Sector of Uniform Thickness

Title: Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 6. The Plate Problem for a Cantilever Sector of Uniform Thickness
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: AF TR 5761 Part 6
Index Price: $0.00
Report Availability: Not available via Contrails
Creator: Williams, M. L.
Date: 1950
Extent: 120
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Identifier: AD0093233
Contract: W33-038-ac-16961
Distribution Classification: 2
Date Issued: 1950-11-01
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report