columbus · Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 11. An Experimental Investigation of Stresses and Deflections in a Swept Thick-Walled Box Beam

Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 11. An Experimental Investigation of Stresses and Deflections in a Swept Thick-Walled Box Beam

Title: Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 11. An Experimental Investigation of Stresses and Deflections in a Swept Thick-Walled Box Beam
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: AF TR 5761 Part 11
Index Price: $0.00
Report Availability: Not available via Contrails
Creator: Williams, M. L.; Hrebec, G. M.
Date: 1950
Date Issued: 1950-09-01
Extent: 70
Corporate Author: Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Identifier: AD0091384
Contract: W33-038-ac-16961
Distribution Classification: 2
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report