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Modeling procedures for handling qualities evaluation of flexible aircraftThis paper presents simplified modeling procedures to evaluate the impact of flexible modes and the unsteady aerodynamic effects on the handling qualities of Supersonic Cruise Aircraft (SCR). The modeling procedures involve obtaining reduced order transfer function models of SCR vehicles, including the important flexible mode responses and unsteady aerodynamic effects, and conversion of the transfer function models to time domain equations for use in simulations. The use of the modeling procedures is illustrated by a simple example.
Document ID
19820030433
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Govindaraj, K. S.
(Calspan Advanced Technology Center Buffalo, NY, United States)
Eulrich, B. J.
(Calspan Advanced Technology Center Buffalo, NY, United States)
Chalk, C. R.
(Calspan Advanced Technology Center Buffalo, NY, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1981
Subject Category
Aircraft Stability And Control
Accession Number
82A13968
Funding Number(s)
CONTRACT_GRANT: F33615-79-C-3618
Distribution Limits
Public
Copyright
Other

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