Custer Channel Wings for Short Takeoff and Landing of Unmanned Aircraft-Reference-Cited by-同舟云学术

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Custer Channel Wings for Short Takeoff and Landing of Unmanned Aircraft

Published:2022-01 Issue:1 Volume:59 Page:196-205
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Mihalik Juraj¹^ORCID,Keane Andy J.¹

Affiliation:

1. University of Southampton, Southampton, England SO17 1BJ, United Kingdom

Funder

Engineering and Physical Sciences Research Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C035944

Reference21 articles.

1. YoungD. W. “Test of 1/3-Scale Powered Model of Custer Channel Shaped Wing,” U.S. Army Air Forces TR 5142, U.S. Army Air Force Materiel Command, Wright Field, Dayton, OH, 1944.

2. YoungD. W. “Test of Two Custer Channel Wings Having a Diameter of 37.2 Inches and Lengths of 43 and 17.5 Inches,” U.S. Army Air Forces TR 5568, U.S. Army Air Force Materiel Command, Wright Field, Dayton, OH, 1947.

3. PasamanickJ. “Langley Full-Scale-Tunnel Tests of the Custer Channel Wing Airplane,” NACA RM L53A09, Langley Aeronautical Lab., Langley Field, VA, 1953.

4. GordonY.GunstonB., Soviet X-Planes, Midland Publ., Leicester, England, 2000, p. 13.

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. Performance analysis and flow mechanism of channel wing considering propeller slipstream;Chinese Journal of Aeronautics;2023-11

2. Aerodynamic Flow Control of a Channel Wing;AIAA AVIATION 2023 Forum;2023-06-08

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