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Flight dynamics research for highly agile aircraftThis 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.
Document ID
19910033077
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nguyen, Luat T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
September 1, 1989
Subject Category
Aircraft Stability And Control
Report/Patent Number
SAE PAPER 892235
Accession Number
91A17700
Distribution Limits
Public
Copyright
Other

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