Development of a Novel Low Stored Volume High-Altitude Wing Design

Author:

Kudva Jay1,Scott Matthew1,Jacob Jamey2,Smith Suzanne3,Asheghian Laila1

Affiliation:

1. NextGen Aeronautics

2. Oklahoma State University

3. University of Kentucky

Publisher

American Institute of Aeronautics and Astronautics

Cited by 2 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. Development of a Measurement Device for Micro Gas Flowrate Based on Laminar Flow Element with Micro-Curved Surface;Micromachines;2024-05-17

2. Structural modeling and investigation of cantilever load-bearing mechanism in telescopic wing;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2024-03-15

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