A Fast MDO Tool for Aeroelastic Optimization in Aircraft Conceptual Design
Author:
Affiliation:
1. Politecnico di Milano
2. Royal Institute of Technology (KTH)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-5911
Reference14 articles.
1. 0
2. 3Ardema, M., Chambers, A., Hahn, A., Miura, H., and Moore, M. "Analytical Fuselage and Wing Weight Estimation of Transport Aircraft," Tech. Rep. 110392, NASA, Ames Research Center, Moffett Field, California,May 1996.
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