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Maximized Gust Loads of a Closed-Loop, Nonlinear Aeroelastic System Using Nonlinear Systems TheoryThe problem of computing the maximized gust load for a nonlinear, closed-loop aeroelastic aircraft is discusses. The Volterra theory of nonlinear systems is applied in order to define a linearized system that provides a bounds on the response of the nonlinear system of interest. The method is applied to a simplified model of an Airbus A310.
Document ID
20040087024
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Silva, Walter A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Computer Programming And Software
Report/Patent Number
AIAA Paper 99-1474
Report Number: AIAA Paper 99-1474
Meeting Information
Meeting: 40th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Saint Louis, MO
Country: United States
Start Date: April 12, 1999
End Date: April 15, 1999
Sponsors: American Helicopter Society, Inc., American Society of Civil Engineers, American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, American Society for Composites
Distribution Limits
Public
Copyright
Public Use Permitted.

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