Aeroelastic Stability Analysis of Tailored Pretwisted Wings
Author:
Affiliation:
1. Swansea University, Swansea, Wales SA2 8PP, United Kingdom
2. Shiraz University, 71963-16548 Shiraz, Iran
3. Georgia Institute of Technology, Atlanta, Georgia 30332
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference36 articles.
1. A review of modelling and analysis of morphing wings
2. A Review of Morphing Aircraft
3. Aeroelastic stability characteristics of a composite swept wing withtip weights for an unrestrained vehicle
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