Optimization of rotor performance in hover using a free wake analysis
Author:
Affiliation:
1. Continuum Dynamics, Inc., Princeton, New Jersey 08543
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46013
Reference22 articles.
1. An Analytical Method for Predicting Rotor Wake Geometry
2. An Analytical and Experimental Investigation of Helicopter Rotor Hover Performance and Wake Geometry Characteristics
Cited by 4 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. Rotor blade aerodynamic shape optimization based on high-efficient optimization method;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-07-26
2. A Variational Method for Computing the Optimal Aerodynamic Performance of Conventional and Compound Helicopters;Journal of the American Helicopter Society;2010
3. Optimum Rotor Performance in Skewed Flow Based on Actuator-Disk Theory;27th AIAA Applied Aerodynamics Conference;2009-06-14
4. Minimum-Induced Power Loss of a Helicopter Rotor via Circulation Optimization;Journal of Aircraft;2004-01
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