Wind Tunnel Evaluation of Powered Static Aerodynamics of an Aerobatic UAV-Reference-Cited by-同舟云学术

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Wind Tunnel Evaluation of Powered Static Aerodynamics of an Aerobatic UAV

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Ol Michael¹,Zeune Cale¹,White Trenton¹,Kudla Thomas¹

Affiliation:

1. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-241

Reference8 articles.

1. Cord,T. "SkyToteAdvancedCargoDeliverySystem". AIAA2003-2753.

2. Owens,D.B.,Cox,D.E.,andMorelli,E.A. "DevelopmentofaLow-CostSub-ScaleAircraftfor FlightResearch: theFASERProject. AIAA2006-3306.

3. Selig,M. "ModelingFull-EnvelopeAerodynamicsofSmallUAVsinRealtime". AIAA2010-7635.

4. Selig, M. "Modeling Propeller Aerodynamics and Slipstream Effects on Small UAVs in Realtime". AIAA 2010-7938.

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