Flow Measurement Techniques for Rotor Wake Characterization on Free-Flying Helicopters in Ground Effect
Author:
Affiliation:
1. University of Maryland, College Park
2. German Aerospace Center (DLR)
3. University of Stuttgart
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-2107
Reference35 articles.
1. Eulerian Simulation of the Fluid Dynamics of Helicopter Brownout
2. Experimental and numerical examination of a helicopter hovering in ground effect
3. Methodology for Rotorcraft Brownout Mitigation Through Flight Path Optimization
4. Tip Vortex Geometry of a Hovering Helicopter Rotor in Ground Effect
5. Fluid Dynamics of Interacting Blade Tip Vortices with a Ground Plane
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1. Flight Experiments and Numerical Simulations for Investigating Multicopter Flow Field and Structure Deformation;Atmosphere;2023-08-24
2. Practical aspects of designing background-oriented schlieren (BOS) experiments for vortex measurements;Experiments in Fluids;2023-03-18
3. Wake Unsteadiness and Tip Vortex System of Full-Scale Helicopters in Ground Effect;Journal of the American Helicopter Society;2022-01-01
4. BOS-Based Three-Dimensional Reconstruction of Rotor Blade Tip Vortex Positions;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2021
5. A Full-Scale Rotor-Wake Investigation of a Free-Flying Helicopter in Ground Effect Using BOS and PIV;Journal of the American Helicopter Society;2020-07-01
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