Experimental investigation of the parallel vortex-airfoil interaction at transonic speeds
Author:
Affiliation:
1. Polytechnic University, Farmingdale, New York 11735
2. University of Texas at Arlington, Arlington, Texas 76019
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11183
Reference19 articles.
1. Helicopter Noise: State-of-the-Art
2. Some Conclusions from an Investigation of Blade‐Vortex Interaction
3. Rotor-vortex interaction noise
4. Vortex-airfoil interaction tests
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1. Experimental Study of Vortex Dynamics during Blade-Vortex Interactions;52nd Aerospace Sciences Meeting;2014-01-10
2. Refurbishment and Testing Techniques in a Transonic Ludwieg Tunnel;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Numerical Simulation of Two-Dimensional Blade-Vortex Interactions Using the Finite Difference Lattice Boltzmann Method;AIAA Journal;2008-09
4. A Study of BVI Noises by the Finite Difference Lattice Boltzmann Method;13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference);2007-05-21
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