Winglet Toe-Out Angle Optimization for the Gates Learjet Longhorn Wing
Author:
Affiliation:
1. Gates Learjet Corporation, Wichita, Kansas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.57976
Reference8 articles.
Cited by 8 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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