columbus · Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 16. Stress and Deflection Tests on Two Full Span 45 Degree Swept Plates of Different Thickness Distribution With Various Support Conditions

Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 16. Stress and Deflection Tests on Two Full Span 45 Degree Swept Plates of Different Thickness Distribution With Various Support Conditions

Title: Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 16. Stress and Deflection Tests on Two Full Span 45 Degree Swept Plates of Different Thickness Distribution With Various Support Conditions
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: AF TR 5761 Part 16
Index Price: $0.00
Report Availability: Not available via Contrails
Creator: Sechler, E. E.; Beebe, W. M.
Date: 1952
Extent: 106
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Aircraft Laboratory
Identifier: AD0007157
Contract: W33-038-ac-16961
Distribution Classification: 2
Date Issued: 1952-07
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report