In 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.
Overview of Recent Flight Flutter Testing Research at NASA Dryden
1997
30 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamics , Test Facilities & Equipment , Aeroservoelasticity , Flutter , Wavelet analysis , Signal processing , System identification , Flight tests , Research aircraft , Excitation , Frequencies , Vibration effects , Stability , Prediction analysis techniques , Time dependence , F-18 aircraft