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Design procedures for flutter-free surface panelsAn approach for the design of lightweight external surface panel configurations to preclude panel flutter was developed. Design procedures were developed for flat orthotropic panels under the interacting influence of parameters such as support flexibility, inplane loads, pressure differential, and flow angularity. The basic relationships required to define these design procedures were based on theoretical panel flutter analyses. Where possible, the design procedures were verified through comparison with available experimental panel flutter data.
Document ID
19770013540
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Laurenson, R. M. (McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Mcpherson, J. I. (McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1977
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-2801
Accession Number
77N20484
Funding Number(s)
CONTRACT_GRANT: NAS1-12436
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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