NASA NTRS · 19640007102
A forced-oscillation method for dynamic- stability testing
Abstract
Small-amplitude forced oscillation technique for determining damping and oscillatory stability in roll, pitch, and yaw in free flight
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Averett, B. T., Kilgore, R. A.. 1964-03-10. A forced-oscillation method for dynamic- stability testing. https://ntrs.nasa.gov/citations/19640007102
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