columbus · Theoretical and Experimental Effect of Sweep upon Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 10. Stresses and Deflection of Unswept and Swept Thin-Walled Beams

Theoretical and Experimental Effect of Sweep upon Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 10. Stresses and Deflection of Unswept and Swept Thin-Walled Beams

Title: Theoretical and Experimental Effect of Sweep upon Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 10. Stresses and Deflection of Unswept and Swept Thin-Walled Beams
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: AF TR 5761 Part 10
Index Price: $0.00
Report Availability: Not available via Contrails
Creator: Dixon, H. H.
Date: 1951
Extent: 130
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Aircraft Laboratory
Identifier: AD0154242
Contract: W33-038-ac-16961
Distribution Classification: 2
Date Issued: 1951-12
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report