Axial wavenumber measurements in axisymmetric jets
Author:
Affiliation:
1. Texas A&M University, College Station, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8151
Reference14 articles.
1. Jet Noise and Shear Flow Instability Seen From an Experimenter’s Viewpoint
2. Influence of Mach number on coherent structure relevant to jet noise
3. A time-domain analysis of the large-scale flow structure in a circular jet. Part 1. Moderate Reynolds number
4. Spatial waves in turbulent jets
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1. Dynamics of free jets submitted to upstream acoustic modulations;Physics of Fluids;2007-01
2. Dynamics of Free Jets Modulated by Plane Acoustic Waves : Part 2. Numerical Simulations;12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference);2006-05-08
3. Measurements in the field of a spark excited compressible axisymmetric jet;Experiments in Fluids;1989-10
4. Spectral cascade and phase distribution of coherent structure in an incompressible circular jet;1st National Fluid Dynamics Conference;1988-07-25
5. Compressibility effects upon the coherent structure of axisymmetric jets;24th Aerospace Sciences Meeting;1986-01-06
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