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Overview of Recent Flight Flutter Testing Research at NASA DrydenIn response to the concerns of the aeroelastic community, NASA Dryden Flight Research Center, Edwards, California, is conducting research into improving the flight flutter (including aeroservoelasticity) test process with more accurate and automated techniques for stability boundary prediction. The important elements of this effort so far include the following: (1) excitation mechanisms for enhanced vibration data to reduce uncertainty levels in stability estimates; (2) investigation of a variety of frequency, time, and wavelet analysis techniques for signal processing, stability estimation, and nonlinear identification; and (3) robust flutter boundary prediction to substantially reduce the test matrix for flutter clearance. These are critical research topics addressing the concerns of a recent AGARD Specialists' Meeting on Advanced Aeroservoelastic Testing and Data Analysis. This paper addresses these items using flight test data from the F/A-18 Systems Research Aircraft and the F/A-18 High Alpha Research Vehicle.
Document ID
19970015518
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Brenner, Martin J.
(NASA Dryden Flight Research Center Edwards, CA United States)
Lind, Richard C.
(NASA Dryden Flight Research Center Edwards, CA United States)
Voracek, David F.
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-4792
H-2165
NAS 1.15:4792
AIAA Paper 97-1023
Meeting Information
Meeting: Structures, Structural Dynamics, and Materials
Location: Kissimmee, FL
Country: United States
Start Date: April 7, 1997
End Date: April 10, 1997
Sponsors: American Society of Mechanical Engineers, American Society of Civil Engineers, American Inst. of Aeronautics and Astronautics, American Helicopter Society, Inc., Alpha STAR Corp.
Accession Number
97N18349
Funding Number(s)
PROJECT: RTOP 522-32-34
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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