Rotor hover performance prediction using a free-wake, computational fluid dynamics method
Author:
Affiliation:
1. Flow Analysis, Inc., Mountain View, California
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45887
Reference14 articles.
1. An Analytical and Experimental Investigation of Helicopter Rotor Hover Performance and Wake Geometry Characteristics
2. A Prescribed Wake Lifting Surface Hover Performance Analysis
3. Conservative full-potential model for unsteady transonic rotor flows
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2. Aerodynamic Noise Analysis Using the Permeable Surface for UH-1H Rotor Blade in Hovering Flight Condition;Journal of the Korean Society for Aeronautical & Space Sciences;2018-05-31
3. A New Coupled Free Wake-CFD Method for Calculation of Helicopter Rotor Flow-Field in Hover;Journal of Aerospace Technology and Management;2014-05-28
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