Cavity Tone Suppression Using a Rod in Cross Flow: investigation of Shear Layer Stability Mechanism
Author:
Affiliation:
1. Illinois Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-700
Reference45 articles.
1. Sound Radiation from Aircraft Wheel-WelVLanding-Gear Configurations
2. Active Store Trajectory Control in Supersonic Cavities Using Microjets and Low-Order Modeling
3. Experimental transition investigation of a free-shear layer above a cavity at Mach 3.5
4. Numerical simulation of the convective instability in a dump combustor
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1. Shallow flow past a cavity: attenuation of oscillations via a bed perturbation;Environmental Fluid Mechanics;2014-07-02
2. Control of Flow Over a Rectangular Cavity Using a Rod in Cross Flow: Further Evaluation of Key Mechanisms;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
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