Improving Ducted Fan UAV Aerodynamics in Forward Flight-Reference-Cited by-同舟云学术

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Improving Ducted Fan UAV Aerodynamics in Forward Flight

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Graf Will¹,Fleming Jonathan²,Ng Wing²

Affiliation:

1. U.S. Air Force

2. Techsburg, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-430

Reference12 articles.

1. Aerodynamic design considerations for a free-flying ducted propeller

2. 4Grunwald, K. J., and Goodson, K. W. "Division of Aerodynamic Loads on a Semispan Tilting-Ducted-Propeller Model in Hovering and Transistion Flight", NASATND-1257,NASA Langley,1962.

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