Optimising Aspects of Rotor Blades in Forward Flight-Reference-Cited by-同舟云学术

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Optimising Aspects of Rotor Blades in Forward Flight

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Johnson Catherine¹,Barakos George¹

Affiliation:

1. University of Liverpool

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1194

Reference34 articles.

1. Numerical optimization of helicopter rotor aerodynamic performance in hover

2. Aerodynamic Shape Optimization of Hovering Rotor Blades Using a NLFD Approach

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Examination of Fixed-Pitch Quadrotor Performance in a Slalom Maneuver Using Inverse Simulation;International Journal of Aeronautical and Space Sciences;2022-09-26

2. Research on the forward flight performance of rotor based on variable-droop leading edge;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2021-06

3. Optimization of Leading Edge Tubercles Applied to Helicopter Rotor Blades;AIAA Scitech 2021 Forum;2021-01-04

4. Blade planform improvement and airfoil shape optimization of helicopters in hover flight;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2020-07-18

5. Variable-Fidelity Methodology for the Aerodynamic Optimization of Helicopter Rotors;AIAA Journal;2019-08

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