This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Structural Considerations for Variable Sweep Wings
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1967 by SAE International in United States
Annotation ability available
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.
|Technical Paper||Fatigue Analysis of an Aircraft Wing Spar|
|Technical Paper||Aircraft-Propeller Development and Testing Summarized|
|Technical Paper||Drag Evaluation of the Bellanca Skyrocket II|
CitationHarvey, J., "Structural Considerations for Variable Sweep Wings," SAE Technical Paper 670881, 1967, https://doi.org/10.4271/670881.
- BaalsD. D.PolhamusE. C. “Variable Sweep Aircraft.” Astronautics and Aerospace Engineering, June 1963, pp. 12-19.
- WhiteRichard “Evaluation of Teflon Liner Wear Surface Bearings.” McDonnell Laboratory Report No. 604-199. 10, Feb. 20, 1967.