Experimental and numerical investigation of a counter rotating open rotor flow field
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. Airbus
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3184
Reference19 articles.
1. Particle Image Velocimetry
2. Investigation of the Propeller Slipstream with Particle Image Velocimetry
3. Flowfield Investigation at Propeller Thrust Reverse
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