Vortex Approach for Downwash and Outwash of Tandem Rotors in Ground Effect
Author:
Affiliation:
1. Nanjing Tech University, 211816 Nanjing, People’s Republic of China
2. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom
Funder
National Natural Science Foundation of China
Natural Science Foundation of Jiangsu Province
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034740
Reference38 articles.
1. Vortical Sheet Behavior in the Wake of a Rotor in Ground Effect
2. Numerical Simulations and Measurements of the Helicopter Wake in Ground Effect
3. Fluid Dynamics of Interacting Blade Tip Vortices with a Ground Plane
4. Flow Environment and Organized Turbulence Structures Near a Plane Below a Rotor
5. Using Model-Scale Tandem-Rotor Measurements in Ground Effect to Understand Full-Scale CH-47D Outwash
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