Effect of Duct-Rotor Aerodynamic Interactions on Blade Design for Hover and Axial Flight-Reference-Cited by-同舟云学术

Effect of Duct-Rotor Aerodynamic Interactions on Blade Design for Hover and Axial Flight

Published:2015-01-03 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Jimenez Benjamin G.¹,Singh Rajneesh²

Affiliation:

1. Oak Ridge Institute for Science and Education

2. Army Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1030

Reference29 articles.

1. 4Pereira, J. L., Hover and Wind-Tunnel Testing of Shrouded Rotors for Improved Micro Air Vehicle Design, Ph.D. thesis,University of Maryland, College Park, Aug. 2008.

2. 5Ohanian, III, O. J., Ducted Fan Aerodynamics and Modeling, with Applications of Steady and Synthetic Jet Flow Control, Ph.D. thesis,Virginia Polytechnic Institute and State University, May 2011.

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