Characterization of the near wake of a helicopter rotor
Author:
Affiliation:
1. Georgia Inst. of Technology, Atlanta
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2909
Reference11 articles.
1. Measurements of the near wake of a rotor in forward flight
2. Vortex-surface collision - 3-D core flow effects
3. McAlister, K. W., and Takahashi, R. K. " NACA 0015 Wing Pressure and TrailingVortex Measurements", NASA Technical Paper 3151, AVSCOM Technical Report 91-A-003.
4. Axial flow in trailing line vortices
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1. Analysis on three-dimensional flow characteristics of rotor wake;AIP Advances;2023-06-01
2. Wake Vortex Definition for Accurate BVI and Broadband Noise Prediction;9th AIAA/CEAS Aeroacoustics Conference and Exhibit;2003-05-12
3. Measurements of the near wake of a rotor in forward flight;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12
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