Boundary Layer Flow Control with a One Atmosphere Uniform Glow Discharge Surface PlasmaLow speed wind tunnel data have been acquired for planar panels covered by a uniform, glow-discharge surface plasma in atmospheric pressure air known as the One Atmosphere Uniform Glow Discharge Plasma (OAUGDP). Streamwise and spanwise arrays of flush, plasma-generating surface electrodes have been studied in laminar, transitional, and fully turbulent boundary layer flow. Plasma between symmetric streamwise electrode strips caused large increases in panel drag, whereas asymmetric spanwise electrode configurations produced a significant thrust. Smoke wire flow visualization and mean velocity diagnostics show the primary cause of the phenomena to be a combination of mass transport and vortical structures induced by strong paraelectric ElectroHydroDynamic (EHD) body forces on the flow.
Document ID
19980022683
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
J Reece Roth (University of Tennessee at Knoxville Knoxville, Tennessee, United States)
Daniel M Sherman (University of Tennessee at Knoxville Knoxville, Tennessee, United States)
Stephen P Wilkinson (Langley Research Center Hampton, Virginia, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Publication Information
Publication: 36th AIAA Aerospace Sciences Meeting and Exhibit
Publisher: American Institute of Aeronautics and Astronautics