Low-Dimensional Modeling of a Mach 0.6 Axisymmetric Jet
Author:
Affiliation:
1. Syracuse University
2. Spectral Energies, LLC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0245
Reference21 articles.
1. Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9
2. Noise-source turbulence statistics and the noise from a Mach 0.9 jet
3. Current Status of Jet Noise Predictions Using Large-Eddy Simulation
4. Using large eddy simulation to explore sound-source mechanisms in jets
5. Application of multipoint measurements for flow characterization
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1. The Design and Validation of a Thermal Boundary Layer Wall Plate;Journal of Fluids Engineering;2019-06-07
2. Repairing Occluded Data for a Mach 0.6 Jet via Data Fusion;AIAA Journal;2017-01
3. Flow Structures Associated with Turbulent Mixing Noise and Screech Tones in Axisymmetric Jets;Flow, Turbulence and Combustion;2016-11-03
4. Large-Eddy Simulation of Plasma-Based Active Control on Imperfectly Expanded Jets;Journal of Fluids Engineering;2016-04-22
5. Comparison of Spatial and Temporal Resolution on High Speed Axisymmetric Jets;53rd AIAA Aerospace Sciences Meeting;2015-01-03
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