Blade Tip Vortex System of a Rotor with Cyclic Pitch
Author:
Affiliation:
1. DLR, German Aerospace Center, D-37073 Göttingen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference29 articles.
1. GrayR. B. “An Aerodynamic Analysis of a Single Bladed Rotor in Hovering and Low Speed Forward Flight as Determined from Smoke Studies of the Vorticity Distribution in the Wake,” Princeton Univ. TR 356, Princeton, NJ, 1956.
2. Rotor Wake Development During the First Revolution
3. Turbulent Tip Vortex Measurements Using Dual-Plane Stereoscopic Particle Image Velocimetry
4. PIV Measurements in the Wake of a Full-Scale Rotor in Forward Flight
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