High-Supersonic/Hypersonic Flutter of Prismatic Composite Plate/Shell Panels
Author:
Affiliation:
1. Loughborough University, Loughborough,England LE11 3TU, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3489
Reference18 articles.
1. Theoretical considerations of panel flutter at high supersonic Mach numbers.
2. Panel flutter - A review of the aeroelastic stability of plates and shells
3. 3Dowell, E. H., Aeroelasticity of Plates and Shells, 1st ed., Noordhoff International,Leyden, The Netherlands, 1975, pp.1-139.
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2. Exact eigensolutions for flutter of two-dimensional symmetric cross-ply composite laminates at high supersonic speeds;Composite Structures;2018-01
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