Flutter Analysis of Laminated Curvilinear-Stiffened Plates
Author:
Affiliation:
1. Embry–Riddle Aeronautical University, Daytona Beach, Florida 32114
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J055021
Reference23 articles.
1. HirschelE. H.PremH.MadelungG., Aeronautical Research in Germany—From Lilienthal Until Today, Springer, Berlin, 2003, p. 280
2. A study on the aero-elastic flutter of stiffened laminated composite panel in the supersonic flow
3. WrightJ. R.CooperJ. E., Introduction to Aircraft Aeroelasticity and Loads, AIAA, Reston, VA, 2007, p. 1
4. Finite element flutter analysis of composite skew panels
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