Nearfield observations of tones generated from supersonic jet flows
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-706
Reference33 articles.
1. On the Noise Emanating from a Two-Dimensional Jet Above the Critical Pressure
2. On the Mechanism of Choked Jet Noise
3. In-flight shock cell noise
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1. Acoustic Effect of Chevrons on Supersonic Jets Exiting Conical Convergent-Divergent Nozzles;AIAA Journal;2012-11
2. Scale-Resolving Simulation of an Unsteady Turbulent Flow and Acoustic Field of a Screeching Supersonic Jet;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04
3. Mode Switching of Jet Noise Screech;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04
4. Numerical Simulation of Three-Dimensional Jet Screech Tones using a General Purpose Finite-Volume CFD code;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
5. Numerical Simulation of Axisymmetric Jet Screech Tones Using a General Purpose Finite-Volume CFD Code;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
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