Synthetic Jets in Quiescent AirAn oscillatory jet with zero net mass flow is generated by a cavity-pumping actuator. Among the three test cases selected for the Langley CFD validation workshop to assess the current CFD capabilities to predict unsteady flow fields, this basic oscillating jet flow field is the least complex and is selected as the first test case. Increasing in complexity, two more cases studied include jet in cross flow boundary layer and unsteady flow induced by suction and oscillatory blowing with separation control geometries. In this experiment, velocity measurements from three different techniques, hot-wire anemometry, Laser Doppler Velocimetry (LDV) and Particle Image Velocimetry (PIV), documented the synthetic jet flow field. To provide boundary conditions for computations, the experiment also monitored the actuator operating parameters including diaphragm displacement, internal cavity pressure, and internal cavity temperature.
Document ID
20070031090
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Yao, C. S. (NASA Langley Research Center Hampton, VA, United States)
Chen, F. J. (NASA Langley Research Center Hampton, VA, United States)
Neuhart, D. (NASA Langley Research Center Hampton, VA, United States)
Harris, J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
April 1, 2007
Publication Information
Publication: Proceedings of the 2004 Workshop on CFD Validation of Synthetic Jets and Turbulent Separation Control
IDRelationTitle20070031059Collected WorksProceedings of the 2004 Workshop on CFD Validation of Synthetic Jets and Turbulent Separation Control20070031059Collected WorksProceedings of the 2004 Workshop on CFD Validation of Synthetic Jets and Turbulent Separation Control