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A Reduced-Order Model for Efficient Simulation of Synthetic Jet ActuatorsA new reduced-order model of multidimensional synthetic jet actuators that combines the accuracy and conservation properties of full numerical simulation methods with the efficiency of simplified zero-order models is proposed. The multidimensional actuator is simulated by solving the time-dependent compressible quasi-1-D Euler equations, while the diaphragm is modeled as a moving boundary. The governing equations are approximated with a fourth-order finite difference scheme on a moving mesh such that one of the mesh boundaries coincides with the diaphragm. The reduced-order model of the actuator has several advantages. In contrast to the 3-D models, this approach provides conservation of mass, momentum, and energy. Furthermore, the new method is computationally much more efficient than the multidimensional Navier-Stokes simulation of the actuator cavity flow, while providing practically the same accuracy in the exterior flowfield. The most distinctive feature of the present model is its ability to predict the resonance characteristics of synthetic jet actuators; this is not practical when using the 3-D models because of the computational cost involved. Numerical results demonstrating the accuracy of the new reduced-order model and its limitations are presented.
Document ID
20040040163
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Yamaleev, Nail K.
(North Carolina Agricultural and Technical State Univ. Greensboro, NC, United States)
Carpenter, Mark H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 2003
Subject Category
Aerodynamics
Report/Patent Number
L-18331
NASA/TM-2003-212664
Report Number: L-18331
Report Number: NASA/TM-2003-212664
Funding Number(s)
WORK_UNIT: WU 23-762-20-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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