Aeroelastic Response of Composite Helicopter Rotor with Random Material Properties
Author:
Affiliation:
1. Indian Institute of Science, Bangalore 560 012, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.30180
Reference39 articles.
1. Preface
2. Free vibration of composite cylindrical panels with random material properties
3. Analysis of composite plates with random material characteristics
4. Buckling of composite circular cylindrical shells with random material properties
5. Forced nonlinear vibration of laminated composite plates with random material properties
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