Numerical simulation of effects of active flow control on an aero-engine inlet
Author:
Affiliation:
1. Key Laboratory of Aircraft Environment Control and Life Support, MIIT Nanjing University of Aeronautics and Astronautics,Nanjing,China
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9695521/9695500/09695878.pdf?arnumber=9695878
Reference11 articles.
1. Flow Control in a Diffusing S-Duct[C];vakili;AIAA ShearFlow Control Conference,2013
2. Boundary Layer Ingestion Propulsion Benefit for Transport Aircraft
3. An experimental study of vortex generators in boundary layer ingesting diffusers with a centerline offset
4. Serpentine inlet performance enhancement using vortex generator based flow control;shu;Chinese Journal of Aeronautics,2006
5. Optimal Design of Passive Flow Control for a Boundary-Layer-Ingesting Offset Inlet Using Design-of-Experiments
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