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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

Authors :
Curtiss, H. C., Jr
Komatsuzaki, T
Traybar, J. J
Publication Year :
1979
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1979.

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.

Details

Language :
English
Database :
NASA Technical Reports
Notes :
NSG-2181
Publication Type :
Report
Accession number :
edsnas.19790018954
Document Type :
Report