columbus · Theoretical and Experimental Effect of Sweep upon Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 2. Stress and Deflection Analysis of Swept Plates

Theoretical and Experimental Effect of Sweep upon Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 2. Stress and Deflection Analysis of Swept Plates

Title: Theoretical and Experimental Effect of Sweep upon Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 2. Stress and Deflection Analysis of Swept Plates
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: AF TR 5761 Part 2
Index Price: $0.00
Report Availability: Not available via Contrails
Creator: Fung, Yung-Cheng
Date: 1949
Date Issued: 1949-12-01
Extent: 115
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