Winglet Shape and Load Optimization with a Numerically Supported Lifting Line Method
Author:
Affiliation:
1. DLR, German Aerospace Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-5902
Reference5 articles.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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