columbus · Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 9. On the Stresses in Cantilever Plates of Arbitrary Planform and Variable Thickness (A Relaxation Procedure With Applications to the Swept Wing Problem)

Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 9. On the Stresses in Cantilever Plates of Arbitrary Planform and Variable Thickness (A Relaxation Procedure With Applications to the Swept Wing Problem)

Title: Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 9. On the Stresses in Cantilever Plates of Arbitrary Planform and Variable Thickness (A Relaxation Procedure With Applications to the Swept Wing Problem)
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: AF TR 5761 Part 9
Index Price: $0.00
Report Availability: Not available via Contrails
Date: 1950
Date Issued: 1950-10-01
Extent: 127
Corporate Author: Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Corporate Report Number: AD0108567
Contract: W33-038-ac-16961
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report
Creator: Fung, Y. C.