Simulation of Sweep-Jet Flow Control, Single Jet and Full Vertical Tail
Author:
Affiliation:
1. Science and Technology Corporation
2. University of California, Santa Cruz
3. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0569
Reference21 articles.
1. 3Andino, M.Y., Lin, John C., Washburn, A.E., Whalen, E.A., Graff, E., Wygnanski, I.J. “Flow Separation Control on a Full-Scale Vertical Tail Model using Sweeping Jet Actuators” AIAA 2015-0785
2. 4Bres, G., Fares, E., Williams, D., and Colonius, T. “Numerical Simulations of the Transient Flow Response of a 3D, Low-Aspect-Ratio Wing to Pulsed Actuation,” AIAA-2011-3440.
3. 5DeSalvo, M., Whalen, E., and Glezer, A. “High-Lift Enhancement using Fluidic Actuation,” AIAA-2010-0863.
4. 7Gokoglu, S., Kuczmarski, M., Culley, D., and Raghu, S. “Numerical Studies of a Fluidic Diverter for Flow Control,” AIAA2009-4012.
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