Jig-Shape Static Aeroelastic Wing Design Problem: A Decoupled Approach
Author:
Affiliation:
1. PTC Global Services, Parsippany, New Jersey 07054
2. Rutgers University, Piscataway, New Jersey 08854
3. Northrup Grumman Corporation, Bethpage, New York 11714-3580
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3035
Reference27 articles.
1. AEROELASTIC CHALLENGES FOR A HIGH SPEED CIVIL TRANSPORT
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4. Combined aerodynamic and structural optimization of a high-speed civil transport wing
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