Parameterization of Temporal Structure in the Single Dielectric Barrier Aerodynamic Plasma Actuator
By C. Enloe, Thomas McLaughlin, Gabriel I. Font, James W. Baughn. 2006
157 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Electrical and Electronic Engineering, Radiology, Nuclear Medicine and Imaging
View Paper: https://www.semanticscholar.org/paper/3b263800090d9d1e7a06336f179e441ae4f78753
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In Aerospace Engineering
In Electrical and Electronic Engineering
In Radiology, Nuclear Medicine and Imaging
Citations in the corpus
- High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator (2010, methodology): “In this work, we choose the profile containing maximum velocity (x = 35 mm) fitted with a skewed Gaussian analytical function to quantify the time-mean momentum addition, J=q 1⁄4 1 0 U(2)dy, using a constant density assumption expected to be accurate within 2% of the background (Enloe et al. 2006; G”
- Simulations of Flow Separation Control using Plasma Actuators (2006, unknown): “Experimental results 16,18,19 suggest that this distribution is similar to a half Gaussian distribution given by 2 2 for 0 x ≥ .”
- Experimental Study for Momentum Transfer in a Dielectric Barrier Discharge Plasma Actuator (2008, background): “The difference in the thrust level between the pure nitrogen gas and air agrees with the previously reported result [22] in which the influence of molecular oxygen in air was intensively investigated.”