Structural Considerations for Variable Sweep Wings

670881

02/01/1967

Event
Aeronautic and Space Engineering and Manufacturing Meeting
Authors Abstract
Content
Pivot point concepts for fighter type aircraft with variable sweep wings are reviewed. Structural and aerodynamic considerations involved in sweep pivot location, a summary of endurance testing of Teflon lined journal bearings, and variation of fatigue life of the aircraft versus wing sweep position are discussed.
Meta TagsDetails
DOI
https://doi.org/10.4271/670881
Pages
8
Citation
Harvey, J., "Structural Considerations for Variable Sweep Wings," SAE Technical Paper 670881, 1967, https://doi.org/10.4271/670881.
Additional Details
Publisher
Published
Feb 1, 1967
Product Code
670881
Content Type
Technical Paper
Language
English