This paper highlights recent results of research conducted at the NASA Langley Research Center as part of a broad flight dynamics program aimed at developing technology that will enable future combat aircraft to achieve greatly enhanced agility capability at subsonic combat conditions. Studies of advanced control concepts encompassing both propulsive and aerodynamic approaches are reviewed. Dynamic stall phenomena and their potential impact on maneuvering performance and stability are summarized. Finally, issues of mathematical modeling of complex aerodynamics occurring during rapid, large amplitude maneuvers are discussed.
Flight dynamics research for highly agile aircraft
1989-09-01
Conference paper
No indication
English
Numerical Investigation of the Flight Dynamics of an Agile Aircraft
British Library Conference Proceedings | 2005
|Flight Dynamics of Highly Flexible Aircraft
AIAA | 2008
|Flight Dynamics of Highly Flexible Aircraft
Online Contents | 2008
|