Nozzle-Exit Boundary-Layer Effects on a Controlled Supersonic Jet
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, Ohio State University, Columbus, Ohio 43210
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053615
Reference41 articles.
1. Effect of initial condition on subsonic jet noise
2. Effect of nozzle exit conditions on subsonic jet noise
3. Roles of initial condition and vortex pairing in jet noise
4. Mode spectra of natural disturbances in a circular jet and the effect of acoustic forcing
5. Effect of Nozzle-Exit Boundary Layer on Jet Noise
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