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David F. Voracek

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Ground vibration and flight flutter tests of the single-seat F-16XL aircraft with a modified wing

by David F. Voracek First published in 1993
4 editions

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The effects of excitation waveforms and shaker moving mass on the measured modal characteristics of a 2- by 5-foot aluminum plate

by David F. Voracek First published in 1989
1 edition

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Buffet induced structural/flight-control system interaction of the X-29A aircraft

by David F. Voracek First published in 1991
1 edition

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Monitoring techniques for the X-29A aircraft's high-speed rotating power takeoff shaft

by David F. Voracek First published in 1990
1 edition

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OLID: OL4666391A

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