Active Damping of Sting Vibrations in Transonic Wind Tunnel Testing-Reference-Cited by-同舟云学术

Active Damping of Sting Vibrations in Transonic Wind Tunnel Testing

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Balakrishna Sundareswara¹,Butler David¹,White Eugene¹,Kilgore William²

Affiliation:

1. ViGYAN, Inc.

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-840

Reference7 articles.

1. Young, C.P., Popernack,T.G., and Gloss, B.B. "National Transonic Facility Model andModel Support Vibration Problems". AIAA-1990-1416.

2. Kilgore,W.A., Balakrishna, S., and Butler, D.H."Reduction of Tunnel Dynamics at theNational Transonic Facility". AIAA- 2001-1162.

3. Igoe, W.B. and Capone, F.T. "Reduction of Wind Tunnel Model Vibrationby Means of a Tuned Damped Vibration Absorber Installed in a Model". NASA TMX-1606, July1968.

4. Freymann, R. "Passive and active damping augmentation systems in the fields of structural dynamics and Acoustics", AIAA-1989-1196.

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