T-tail flutter: Potential-flow modelling, experimental validation and flight tests (2014)
Attributed to:
Nonlinear Flexibility Effects on Flight Dynamics and Control of Next-Generation Aircraft
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1016/j.paerosci.2014.07.002
Publication URI: http://dx.doi.org/10.1016/j.paerosci.2014.07.002
Type: Journal Article/Review
Parent Publication: Progress in Aerospace Sciences