Aeroservoelastic wind-tunnel investigations using the active flexible wing model - Status and recent accomplishments-Reference-Cited by-同舟云学术

Aeroservoelastic wind-tunnel investigations using the active flexible wing model - Status and recent accomplishments

Published:1989-04-03 Issue: Volume: Page:
ISSN:
Container-title:30th Structures, Structural Dynamics and Materials Conference
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Author:

NOLL THOMAS¹,PERRY, III BOYD¹,TIFFANY SHERWOOD¹,COLE STANLEY¹,BUTTRILL CAREY¹,ADAMS, JR. WILLIAM¹,HOUCK JACOB¹,SRINATHKUMAR S.¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-1168

Reference23 articles.

1. Perry,B.,111;Dunn,H.J.;andSandford,M.C.: ControlLawParameterizationforan Aeroelastic Wind-TunnelModelEquippedwith an ActiveRoll ControlSystemandComparisonwithExperiment. AIAAPaperNo. 88-2211,presentedatthe AIAA 29th Structures,StructuralDynamicsandMaterials Conference,April 1988.

2. Decoupler Pylon: A Simple, Effective Wing/Store Flutter Suppressor

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