Particle Image Velocimetry Measurements and Performance Analysis of Rotors with Slotted Blades
Author:
Affiliation:
1. U.S. Naval Academy Rotorcraft Center, Annapolis, Maryland 21402
Funder
Office of Naval Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034640
Reference50 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,” Tech. Rept. 356, Princeton Univ., Princeton, NJ, Sept. 1956.
2. An Analytical Method for Predicting Rotor Wake Geometry
3. The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor Performance
4. CookC. V. “The Structure of the Rotor Blade Tip Vortex,” Paper 3, Aerodynamics of Rotary Wings, CP-111, AGARD, Neuilly sur Seine, France, Sept. 1972.
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