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The Influence of Feedback on the Aeroelastic Behavior of Tilt Proprotor Aircraft Including the Effects of Fuselage Motion
The Influence of Feedback on the Aeroelastic Behavior of Tilt Proprotor Aircraft Including the Effects of Fuselage Motion
- Publication Year :
- 1979
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1979.
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Abstract
- The influence of single loop feedbacks to improve the stability of the system are considered. Reduced order dynamic models are employed where appropriate to promote physical insight. The influence of fuselage freedom on the aeroelastic stability, and the influence of the airframe flexibility on the low frequency modes of motion relevant to the stability and control characteristics of the vehicle were examined.
- Subjects :
- Aircraft Design, Testing And Performance
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Notes :
- NSG-2181
- Publication Type :
- Report
- Accession number :
- edsnas.19790018954
- Document Type :
- Report