Effects of Plasma Aerodynamic Actuation on Corner Separation in a Highly Loaded Compressor Cascade
Author:
Publisher
IOP Publishing
Subject
Condensed Matter Physics
Link
http://stacks.iop.org/1009-0630/16/i=3/a=13/pdf
Reference23 articles.
1. The Design of Highly Loaded Axial Compressors
2. Flow Mechanism for Stall Margin Improvement due to Circumferential Casing Grooves on Axial Compressors
3. Parametric Study of Tip Clearance—Casing Treatment on Performance and Stability of a Transonic Axial Compressor
4. Separation Control on Low-Pressure Turbine Airfoils Using Synthetic Vortex Generator Jets
5. Aerodynamic Blade Row Interactions in an Axial Compressor—Part I: Unsteady Boundary Layer Development
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3. A Qualitative Comparison of Unsteady Operated Compressor Stator Cascades with Active Flow Control;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2018-08-05
4. A pulsed generator for synchronous discharges of high-energy plasma synthetic jet actuators;IEEE Transactions on Dielectrics and Electrical Insulation;2017
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