Coupling of Twin Supersonic Jets of Complex Geometry
Author:
Affiliation:
1. DYNACS Engineering Company, Brook Park, Ohio 44142
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2523
Reference33 articles.
1. Dynamic pressure loads associated with twin supersonic plume resonance
2. Dynamic loads on twin jet exhaust nozzles due to shock noise
3. Twin-jet screech suppression
4. Twin jet screech suppression concepts tested for 4.7 percent axisymmetric and two-dimensional nozzle configurations
5. Nozzle geometry effects on supersonic jet interaction
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