Optimum Aspect Ratio for Subsonic Air Vehicles

Author:

Takahashi Timothy T.1

Affiliation:

1. Santa Clara University, Santa Clara, California 95053

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference15 articles.

Cited by 12 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

1. Designing high aspect ratio wings: A review of concepts and approaches;Progress in Aerospace Sciences;2024-02

2. High-speed wind tunnel test of the CAE aerodynamic validation model;Chinese Journal of Aeronautics;2018-03

3. Multi-Disciplinary Impact of Engine Parameters Upon Transport Aircraft Climb Fuel Consumption;53rd AIAA Aerospace Sciences Meeting;2015-01-03

4. A Multi-Disciplinary Survey of Energy Maneuverability for Subsonic Endurance Based Aircraft;15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2014-06-13

5. Planform Optimization of a Flying Wing with a Solid Homogeneous Structure;14th AIAA Aviation Technology, Integration, and Operations Conference;2014-06-13

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