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Stability Analysis of Streaks Induced By Optimized Vortex GeneratorsNumerical computations are performed to investigate the potential for transition control in an axisymmetric boundary layer via fully realizable, streamwise stationary streaks induced by an azimuthally periodic array of surface mounted vortex generators (VGs). Previous work has shown that suitable streaks of this type can significantly reduce the growth of Mack’s second mode instabilities, but large streak amplitudes can make the flow susceptible to previously absent streak instabilities that can become the leading cause of transition. Here, we use the adjoint capabilities of the SU2 flow solver to optimize the VG shape to maximize the reduction in the growth of second-mode disturbances while also preventing the streak amplitudes from reaching large enough values to precipitate an earlier onset of transition via streak instabilities. The geometry and the freestream flow conditions are selected to match a relevant trajectory lo-cation from the HIFiRE-1 flight experiment. Results show that the optimized VGs can increase the mean streak amplitude by 117% with respect to a manually developed baseline design. The stability of this optimized basic state is analyzed via the plane-marching parabolized stability equations, predicting a fully laminar flow over the entire cone, or equivalently, yielding transition delay of 130% versus the 17% for the baseline VGs.
Document ID
20220006756
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Connor Klauss
(University of Maryland, College Park College Park, Maryland, United States)
Clark C Pederson
(Langley Research Center Hampton, Virginia, United States)
Pedro Paredes ORCID
(National Institute of Aerospace Hampton, Virginia, United States)
Meelan Choudhari ORCID
(Langley Research Center Hampton, Virginia, United States)
Boris Diskin
(National Institute of Aerospace Hampton, Virginia, United States)
James Baeder
(University of Maryland, College Park College Park, Maryland, United States)
Date Acquired
May 2, 2022
Publication Date
June 27, 2022
Subject Category
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: AIAA AVIATION Forum and Exposition
Location: Chicago, IL
Country: US
Start Date: June 27, 2022
End Date: July 1, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 725017.02.07.03.01
CONTRACT_GRANT: SAA1-31764
CONTRACT_GRANT: NNL09AA00A
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
Boundary layer transition
Hydrodynamic stability
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