Effects of manufacturing parameters on performance of fluidic oscillators for aerodynamic flow control

An investigation is conducted into the effects of dimensional variation, material selection, and manufacturing process on the performance characteristics of a self-oscillating fluidic oscillator. Measurements of oscillation frequency, inlet pressure, and jet profile are performed for actuators having varying nozzle and cavity dimensions. Actuators made of aluminum and carbon fiber reinforced polyetherketoneketone are tested, and the effects of varying manufacturing processes between machining, selective laser sintering, stereolithography, and injection molding are assessed. Models based on dimensionless variables are used to characterize the variation in frequency and inlet pressure for a given mass flow rate. Variation of the nozzle geometry and cavity shoulder width influence the oscillation frequency, and variation of nozzle geometry affects the required driving pressure. Dimensional variations due to manufacturing process tolerances are found to affect actuator performance characteristics, while material selection alone does not affect, provided manufacturing to the required tolerances is possible.

[1]  Viyat Viral Jhaveri,et al.  Effect of dimensional variation, manufacturing process, and material on performance of fluidic oscillator , 2017 .

[2]  Mohamed Gad-el-Hak,et al.  Flow control : fundamentals and practices , 1998 .

[3]  John C. Lin,et al.  An Overview of Active Flow Control Enhanced Vertical Tail Technology Development , 2016 .

[4]  Jose Flich,et al.  Flow Control , 2011, Encyclopedia of Parallel Computing.

[5]  Mehmet N. Tomac Internal Fluid Dynamics and Frequency Characteristics of Feedback-Free Fluidic Oscillators , 2013 .

[6]  M. Amitay,et al.  Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators , 2001 .

[7]  Louis N. Cattafesta,et al.  Actuators for Active Flow Control , 2011 .

[8]  M. Koklu Effect of a Coanda Extension on the Performance of a Sweeping-Jet Actuator , 2016 .

[9]  K. Srinivas,et al.  Computational Fluid Dynamics Analysis of Externally BlownFlap Configuration for Transport Aircraft , 2008 .

[10]  Abigail Kuchan,et al.  The integration of active flow control devices into composite wing flaps , 2012 .

[11]  Michael Meyer,et al.  Towards the Industrial Application of Active Flow Control in Civil Aircraft - An Active Highlift Flap , 2014 .

[12]  Mehmet N. Tomac,et al.  Frequency Studies and Scaling Effects of Jet Interaction in a Feedback-Free Fluidic Oscillator , 2012 .

[13]  James W. Gregory,et al.  Characterization of a Micro Fluidic Oscillator for Flow Control , 2004 .

[14]  M. Desalvo Airfoil Aerodynamic Performance Enhancement by Manipulation of Trapped Vorticity Concentrations using Active Flow Control , 2015 .

[15]  S Sakurai,et al.  Study of the Application of Separation Control by Unsteady Excitation to Civil Transport Aircraft , 1999 .

[16]  James W. Gregory,et al.  A Review of Fluidic Oscillator Development , 2013 .

[17]  M. Amitay,et al.  SYNTHETIC JETS , 2001 .

[18]  James W. Gregory,et al.  Variable-Frequency Fluidic Oscillator Driven by a Piezoelectric Bender , 2009 .

[19]  Corin Gologan,et al.  A Method for the Comparison of Transport Aircraft with Blown Flaps , 2010 .

[20]  Michael Amitay,et al.  Performance Enhancement of a Vertical Tail Using Synthetic Jet Actuators: Flow Physics , 2013 .

[21]  C. Edward Lan,et al.  Airplane Aerodynamics and Performance , 2016 .

[22]  Israel J Wygnanski,et al.  The control of flow separation by periodic excitation , 2000 .