COMPACT FLUIDIC ACTUATOR ARRAYS FOR FLOW CONTROL TECHNICAL ABSTRACT: THE OVERALL OBJECTIVE OF THE PROPOSED…
Award details are derived from public USAspending.gov records. Not a bid recommendation.
Award details
- Award ID
- NNX09CB20C
- Contractor
- Awarding agency
- National Aeronautics and Space Administration
- Sub-agency / office
- National Aeronautics and Space Administration
- Award amount
- $0
- Period of performance
- Jun 24, 2009 – Jan 4, 2011
- NAICS
- 541712 — Research and Development in the Physical, Engineering, and Life Sciences
- PSC
- PSC AR11
- Place of performance
- MD
Public award description
COMPACT FLUIDIC ACTUATOR ARRAYS FOR FLOW CONTROL TECHNICAL ABSTRACT: THE OVERALL OBJECTIVE OF THE PROPOSED RESEARCH IS TO DESIGN, DEVELOP AND DEMONSTRATE FLUIDIC ACTUATOR ARRAYS FOR AERODYNAMIC SEPARATION CONTROL AND DRAG REDUCTION. THESE ACTUATORS ARE BASED ON A COMPACT DESIGN OF LOW MASS-FLOW FLUIDIC OSCILLATORS THAT PRODUCE HIGH FREQUENCY (1-5 KHZ) SWEEPING JETS. PRELIMINARY EXPERIMENTS ON SEPARATION CONTROL OVER A TRAILING EDGE FLAP ON A NACA 0015 AIRFOIL, V-22 WING SECTION FOR DOWNLOAD REDUCTION, CAVITY TONES AND JET THRUST VECTORING HAVE SHOWN ENCOURAGING RESULTS FOR THESE ACTUATORS.
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