Investigation of the Propeller Slipstream with Particle Image Velocimetry
Author:
Affiliation:
1. DLR, German Aerospace Center, 37073 Göttingen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.33917
Reference18 articles.
1. Veldhuis, L. L. M. "Propeller Wing Aerodynamic Interference," Ph.D. Dissertation,Delft University of Technology, Delft, TheNetherlands,2005.
2. Investigation of the near wake of a propeller using particle image velocimetry
3. Three-component velocity field measurements of propeller wake using a stereoscopic PIV technique
4. PIV analysis of flow around a container ship model with a rotating propeller
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