Active flow control to reduce fan blade vibration and noise
Author:
Affiliation:
1. Virginia Polytechnic Inst. and State Univ., Blacksburg
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1806
Reference13 articles.
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2. %aumann, RG. "Control of the Wake from a Simulated Blade by Trailing EdgeBlowing0022, M.S. Thesis,Lehigh Univ.Bethlehem,PA,1992.
3. orcoraa, T.E. "Control of the Wake Tom a Simulated Blade by Trailing EdgeBlowing0022, MS. Thesis,Lehigh Univ.Bethlehem,PA,1992.
4. The effect of jet injection geometry on two-dimensional momentumless wakes
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