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Monitoring techniques for the X-29A aircraft's high-speed rotating power takeoff shaft by Voracek, David F.
Published 1990Call Number: Loading…Connect to online resource
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2
Ground vibration and flight flutter tests of the single-seat F-16XL aircraft with a modified wing by Voracek, David F.
Published 1993Call Number: Loading…
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3
The effects of excitation waveforms and shaker moving mass on the measured modal characteristics of a 2- by 5-foot aluminum plate by Voracek, David F.
Published 1988Call Number: Loading…
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4
Buffet induced structural flight-control system interaction of the X-29A aircraft by Voracek, David F.
Published 1991Call Number: Loading…Click here to view document online
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5
Overview of recent flight flutter testing research at NASA Dryden / by Brenner, Martin J., Lind, Rick, 1968-, Voracek, David F.
Published 1997Call Number: Loading…Online Access
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6
Ground vibration test results of a JetStar airplane using impulsive sine excitation by Kehoe, M. W.
Published 1989Other Authors: “…Voracek, David F.…”
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7
Hybrid damping system for an electronic equipment mounting shelf final report for NASA-Ames university consortium, joint research interchange, February 1, 1995 - January 31, 1997 /
Published 1997Other Authors: “…Voracek, David F.…”
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8
A probabilistic approach to model update by Horta, Lucas G.
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9
Overview of recent flight flutter testing research at NASA Dryden by Brenner, Marty, 1955-
Published 1997Other Authors:Call Number: Loading…Click here to view online
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Related Subjects
Airplanes
Testing
Aeroservoelasticity
Flutter
System identification
Wavelet analysis
Active control
Actuators
Chirp
Circuits
Electronic equipment
Finite element method
Flight testing
Flight tests
Flutter analysis
Frequency response
Grumman X-29A (Research plane)
Probability theory
Research aircraft
Signal processing
Vibration
Vibration damping
Vibration effects
Waves