Coupled-Physics Modeling of Electrostatic Fluid Accelerators for Forced Convection Cooling

Classic thermal management solutions are becoming inadequate and there is an increasing need for fundamentally new approaches. Electrohydrodynamic ionic wind pumps, also known as electrostatic fluid accelerators (EFA), have the potential for becoming a critical element in electronics thermal management solutions. As the EFA field continues to evolve, developing new EFA-based technologies will require accurate models that can help predict pump performance metrics, such as air velocity profile, back pressure, and cooling efficiency. Many previous modeling efforts only account for electrostatic interactions. For truly accurate modeling, however, it is important to include effects of fluid dynamics and space charge diffusion. The modeling problem becomes especially challenging for the design and optimization of EFA devices with greater complexity and smaller dimensions. This paper presents a coupled-physics finite element model (FEM) that accounts for space charge generation from a corona discharge, as well as space charge diffusion and fluid dynamic effects in EFAs. A cantilever EFA structure is modeled and analyzed for forced convection cooling. Numerical modeling predicts maximum air velocities of approximately 7 m/s and a maximum convection heat transfer coefficient of 282 W/(m 2 K) for the cantilever EFA structure investigated. Preliminary experimental results for a microfabriacted cantilever EFA device for forced convection cooling are also discussed.

[1]  G. M. Colver,et al.  Modeling of DC corona discharge along an electrically conductive flat plate with gas flow , 1997 .

[2]  Jen-Shih Chang,et al.  Electromagnetic hydrodynamics , 1994 .

[3]  M. Ohadi,et al.  Thermal management of harsh-environment electronics , 2004, Twentieth Annual IEEE Semiconductor Thermal Measurement and Management Symposium (IEEE Cat. No.04CH37545).

[4]  L. Loeb,et al.  Fundamental Processes of Electrical Discharge in Gases , 1940, Nature.

[5]  D. A. Parker,et al.  Corona driven air propulsion for cooling of electronics , 2003 .

[6]  Eran Sher,et al.  Extinction of pool flames by means of a dc electric field , 1993 .

[7]  F. Peek Dielectric Phenomena in High Voltage Engineering , 2002 .

[8]  James Q. Feng Application of Galerkin Finite-Element Method with Newton Iterations in Computing Steady-State Solutions of Unipolar Charge Currents in Corona Devices , 1999 .

[9]  O. Stuetzer,et al.  Ion Drag Pressure Generation , 1959 .

[10]  Suresh V. Garimella,et al.  Microscale Ion-Driven Air Flow Over a Flat Plate , 2004 .

[11]  Suresh V. Garimella,et al.  Numerical Simulation of Microscale Ion-Driven Air Flow , 2003 .

[12]  A.V. Mamishev,et al.  Design and optimization of electrostatic fluid accelerators , 2006, IEEE Transactions on Dielectrics and Electrical Insulation.

[13]  J. Seyed-Yagoobi,et al.  Theoretical analysis of ion-drag pumping , 1992, Conference Record of the 1992 IEEE Industry Applications Society Annual Meeting.

[14]  James Q. Feng Electrohydrodynamic flow associated with unipolar charge current due to corona discharge from a wire enclosed in a rectangular shield , 1999 .

[15]  Francis Hauksbee,et al.  Physico-mechanical experiments on various subjects , 1970 .

[16]  Eric Moreau,et al.  Effect of a DC corona electrical discharge on the airflow along a flat plate , 2002 .

[17]  A.V. Mamishev,et al.  Numerical simulation and optimization of electrostatic air pumps , 2004, The 17th Annual Meeting of the IEEE Lasers and Electro-Optics Society, 2004. LEOS 2004..