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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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BibTeXRIS

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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