Hub Drag-Reduction Strategies of Canard Rotor/Wing Unmanned Aerial Vehicles
Author:
Affiliation:
1. Korea Aerospace Research Institute, Daejon 305-333, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.24395
Reference7 articles.
1. Canard Rotor/Wing: A Revolutionary High-speed Rotorcraft Concept
2. Fixed-wing performance predictions of the Canard rotor/wing concept based on wind tunnel test results
3. Low-speed wind tunnel test results of the Canard Rotor/Wing concept
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1. Research on Circulation Control System Design of Rotor/Wing Based on CFD;Journal of Aerospace Engineering;2023-01
2. Design and Analysis of Rotor/Wing Flap for Canard Rotor/Wing Aircraft;Journal of Physics: Conference Series;2019-05-01
3. Aerodynamic Analysis of the Rotor/Wing in Conversion Flight;Applied Mechanics and Materials;2014-10
4. Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations;Journal of Aircraft;2013-03
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