Active Flow Control of Separation on a 1/19th and 1/9th Scale Vertical Tail
ORAL
Abstract
Coordinated simulations and experiments are compared on a 1/19thand 1/9thscale vertical tail with and without active flow control (mean aerodynamic chord Re = 350k and 700k respectively). On the larger model, both synthetic and sweeping jet actuators are considered while only synthetic jets were compared on the smaller model. Due to the unsteady nature of the flow control, most of the simulations employ DDES but comparisons are also made to RANS simulations. Since computational efficiency is the prime motivation for using RANS simulations, it is common to replace the unsteady actuation by a steady jet with a concomitant adjustment of the strength. A comparison of the flow fields will be made to provide an assessment of this practice.
*Funding was provided by Boeing Corporation and by the National Science Foundation (CBET) under award number 1710670. This research used resources under an INCITE and an Early Science Project from the Argonne Leadership Computing Facility, which is a DOE Office of Science User Facility supported under Contract DE-AC02-06CH11357.
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Presenters
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Kenneth E Jansen
- Univ of Colorado - Boulder
- Univ. of Colorado - Boulder