Exit-Slot Orientation on Pumping Blades for a Rotor in Ground Effect
Author:
Affiliation:
1. U.S. Naval Academy, Annapolis, Maryland 21402
2. U.S. Navy, Annapolis, Maryland 21402
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033719
Reference53 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. 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,” AGARD Proceedings on Aerodynamics of Rotary Wings, Sept. 1972, Paper 3.
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