Validation of Vortex Propeller Theory for UAV Design with Uncertainty Analysis-Reference-Cited by-同舟云学术

Validation of Vortex Propeller Theory for UAV Design with Uncertainty Analysis

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

Moffitt Blake¹,Bradley Thomas¹,Parekh David²,Mavris Dimitri¹

Affiliation:

1. Georgia Institute of Technology

2. Georgia Tech Research Institute

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-406

Reference20 articles.

1. Crigler, J.L. "Comparison of calculated and experimental propeller characteristics for four-six-and eight-blade single-rotatingpropellers," NACA ACRFebruary1944.

2. Predicting the Contribution of Running Propellers to Aircraft Stability Derivatives

3. Phillips,W.F.,MechanicsofFlight,JohnWileyandSons,Inc.,Hoboken,NewJersey,2004.

4. TanglerJ.L."Thenebulousartofusingwindtunnelaerofoildataforpredictingrotorperformance,"WindEnergy. 2002;5:245-257.

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