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Aeroelastic modeling of the active flexible wing wind-tunnel modelThe primary issues involved in the generation of linear, state-space equations of motion of a flexible wind tunnel model, the Active Flexible Wing (AFW), are discussed. The codes that were used and their inherent assumptions and limitations are also briefly discussed. The application of the CAP-TSD code to the AFW for determination of the model's transonic flutter boundary is included as well.
Document ID
19910013020
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Silva, Walter A. (Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Heeg, Jennifer (NASA Langley Research Center Hampton, VA, United States)
Bennett, Robert M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Publication Information
Publication: Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 2
Subject Category
Aircraft Design, Testing And Performance
Accession Number
91N22333
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19910013018Collected WorksFourth NASA Workshop on Computational Control of Flexible Aerospace Systems, part 219910013018Collected WorksFourth NASA Workshop on Computational Control of Flexible Aerospace Systems, part 2
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