Noise Reduction in a Non-Ideally Expanded Round Jet via Steady Blowing
Author:
Affiliation:
1. Seoul National University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1202
Reference12 articles.
1. Ahuja, K.K. and Brown, W.H., 1989, "Shear flow controlbymechanicaltabs,"AIAAPaper89-0994.
2. Flesberg, S., 2001, "Aeroacoustic Characteristics of Supersonic Rectangular Jets," AIAA Paper No. 2001-0015.
3. Ibrahim, M.K. and Nakamura, Y., 2000, "The Effects of Vane-Type Tabs on Flow ans Acoustic Fields of Supersonic Jet,"AIAAPaperNo.2000-0087.
4. Mixing Enhancement of Compressible Jets by Using Unsteady Microjets as Actuators
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