columbus · "Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity" Part I - "Elastostatic and Aeroelastic Problems Relating to Thin Wings of High-Speed Airplanes"

"Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity" Part I - "Elastostatic and Aeroelastic Problems Relating to Thin Wings of High-Speed Airplanes"

Title: "Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity" Part I - "Elastostatic and Aeroelastic Problems Relating to Thin Wings of High-Speed Airplanes"
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: AF TR 5761 Part 1
Index Price: $0.00
Report Availability: Not available via Contrails
Creator: Fung, Yuan-Cheng
Date: 1949
Date Issued: 1949-02-01
Extent: 127
Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
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