Numerical and Experimental Study of Centrifugally Driven Flow Inside a Rotating Duct
Author:
Affiliation:
1. United Technologies Research Center, East Hartford, Connecticut 06108
2. University of Texas at Austin, Austin, Texas 78712
3. Sikorsky Aircraft, Stratford, Connecticut 06615
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034008
Reference14 articles.
1. Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap
2. Combustion-Powered Actuation for Dynamic-Stall Suppression: High-Mach Simulations and Low-Mach Experiments
3. The Canard Rotor Wing (CRW) Aircraft - A New Way to Fly
4. Modeling Internal Flow Through a Rotating Duct Using Quasi 1-D Euler Equations
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