Research & Technology
Research Focus
Active Flow and Noise Control
Active flow and noise control methods will be employed to enhance the efficiency of commercial and military aircraft through innovative aircraft configurations. As a result future aircraft will be quieter and induce less drag, thereby requiring less fuel and shorter distances for take off and landing, ultimately resulting in quieter and safer airports with higher traffic densities.
Introduction to Active Flow and Noise Control
Applications in Active Flow and Noise Control
Technical Leads
The technical leads for FCAAP's active flow and noise control research are Louis Cattafesta and Lawrence Ukeiley.
Projects
Current research projects in active flow and noise control:
- Virtual Shock Shaping and Design of an Adaptive Supersonic Engine Inlet
- Active and Adaptive Control of Supersonic Flow Using High Bandwidth Pulsed Micro-Actuators (Farrukh Alvi)
- Active Flow Control to Improve Aerodynamic Performance of Turbomachinery Systems (Farrukh Alvi)
- Characterization and Control of Impinging Jets at Realistic Flow Conditions (Brent Greska, Anjaneyulu Krothapalli)
- Airfoil Aeroacoustics: Simulation and Modeling (Christopher Tam)
- Biosynthesis of Aerodynamics Microsystems and Structures (Jonathan Clark, William Oates)
- Intelligent Controlled High Temperature Shape Memory Alloy (SMA) Actuators (Raj Vaidyanathan, Cheryl Xu)
- Grazing Flow Incidence Tube (GFIT) (Mark Sheplak, Lou Cattafesta)
- Characterization of Aeroacoustic Noise Sources for Future Aircraft Design (Lou Cattafesta)
- Plasma Actuated Flow Management (Subrata Roy, Lou Cattafesta and Jay Kapat)
- Massively Parallel Higher-Order Method for Turbulence and Aeroacoustics Simulations (Andreas Haselbacher)
Platforms
Commercial and military platforms utilizing active flow and noise control technologies (click image to enlarge):










